Create the new trunk
This commit is contained in:
Sampo Niskanen
commit
e246eb1f17
11
.classpath
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.classpath
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||||
<?xml version="1.0" encoding="UTF-8"?>
|
||||
<classpath>
|
||||
<classpathentry kind="src" path="src"/>
|
||||
<classpathentry kind="src" path="extra-src"/>
|
||||
<classpathentry kind="con" path="org.eclipse.jdt.launching.JRE_CONTAINER"/>
|
||||
<classpathentry kind="lib" path="/home/sampo/Projects/OpenRocket/lib/miglayout15-swing.jar"/>
|
||||
<classpathentry kind="con" path="org.eclipse.jdt.USER_LIBRARY/JCommon 1.0.16"/>
|
||||
<classpathentry kind="con" path="org.eclipse.jdt.USER_LIBRARY/JFreeChart 1.0.13"/>
|
||||
<classpathentry kind="lib" path="/home/sampo/Projects/OpenRocket/extra-lib/RXTXcomm.jar"/>
|
||||
<classpathentry kind="output" path="bin"/>
|
||||
</classpath>
|
||||
17
.project
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.project
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||||
<?xml version="1.0" encoding="UTF-8"?>
|
||||
<projectDescription>
|
||||
<name>OpenRocket</name>
|
||||
<comment></comment>
|
||||
<projects>
|
||||
</projects>
|
||||
<buildSpec>
|
||||
<buildCommand>
|
||||
<name>org.eclipse.jdt.core.javabuilder</name>
|
||||
<arguments>
|
||||
</arguments>
|
||||
</buildCommand>
|
||||
</buildSpec>
|
||||
<natures>
|
||||
<nature>org.eclipse.jdt.core.javanature</nature>
|
||||
</natures>
|
||||
</projectDescription>
|
||||
4
ChangeLog
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4
ChangeLog
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|
||||
2009-05-24 Sampo Niskanen <sampo.niskanen@iki.fi>
|
||||
|
||||
* Initial release 0.9.0
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||||
|
||||
700
LICENSE.TXT
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700
LICENSE.TXT
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|
||||
OpenRocket - A model rocket simulator
|
||||
|
||||
Copyright (C) 2007-2009 Sampo Niskanen
|
||||
|
||||
This program is free software; you can redistribute it and/or modify
|
||||
it under the terms of the GNU General Public License as published by
|
||||
the Free Software Foundation; either version 3 of the License, or (at
|
||||
your option) any later version.
|
||||
|
||||
This program is distributed in the hope that it will be useful, but
|
||||
WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
|
||||
General Public License (below) for more details.
|
||||
|
||||
|
||||
Additional permission under GNU GPL version 3 section 7:
|
||||
|
||||
The licensors grant additional permission to package this Program, or
|
||||
any covered work, along with any non-compilable data files (such as
|
||||
thrust curves or component databases) and convey the resulting work.
|
||||
|
||||
|
||||
------------------------------------------------------------------------
|
||||
|
||||
|
||||
GNU GENERAL PUBLIC LICENSE
|
||||
Version 3, 29 June 2007
|
||||
|
||||
Copyright (C) 2007 Free Software Foundation, Inc. <http://fsf.org/>
|
||||
Everyone is permitted to copy and distribute verbatim copies
|
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Preamble
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The GNU General Public License is a free, copyleft license for
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|
||||
reasonable ways as different from the original version; or
|
||||
|
||||
d) Limiting the use for publicity purposes of names of licensors or
|
||||
authors of the material; or
|
||||
|
||||
e) Declining to grant rights under trademark law for use of some
|
||||
trade names, trademarks, or service marks; or
|
||||
|
||||
f) Requiring indemnification of licensors and authors of that
|
||||
material by anyone who conveys the material (or modified versions of
|
||||
it) with contractual assumptions of liability to the recipient, for
|
||||
any liability that these contractual assumptions directly impose on
|
||||
those licensors and authors.
|
||||
|
||||
All other non-permissive additional terms are considered "further
|
||||
restrictions" within the meaning of section 10. If the Program as you
|
||||
received it, or any part of it, contains a notice stating that it is
|
||||
governed by this License along with a term that is a further
|
||||
restriction, you may remove that term. If a license document contains
|
||||
a further restriction but permits relicensing or conveying under this
|
||||
License, you may add to a covered work material governed by the terms
|
||||
of that license document, provided that the further restriction does
|
||||
not survive such relicensing or conveying.
|
||||
|
||||
If you add terms to a covered work in accord with this section, you
|
||||
must place, in the relevant source files, a statement of the
|
||||
additional terms that apply to those files, or a notice indicating
|
||||
where to find the applicable terms.
|
||||
|
||||
Additional terms, permissive or non-permissive, may be stated in the
|
||||
form of a separately written license, or stated as exceptions;
|
||||
the above requirements apply either way.
|
||||
|
||||
8. Termination.
|
||||
|
||||
You may not propagate or modify a covered work except as expressly
|
||||
provided under this License. Any attempt otherwise to propagate or
|
||||
modify it is void, and will automatically terminate your rights under
|
||||
this License (including any patent licenses granted under the third
|
||||
paragraph of section 11).
|
||||
|
||||
However, if you cease all violation of this License, then your
|
||||
license from a particular copyright holder is reinstated (a)
|
||||
provisionally, unless and until the copyright holder explicitly and
|
||||
finally terminates your license, and (b) permanently, if the copyright
|
||||
holder fails to notify you of the violation by some reasonable means
|
||||
prior to 60 days after the cessation.
|
||||
|
||||
Moreover, your license from a particular copyright holder is
|
||||
reinstated permanently if the copyright holder notifies you of the
|
||||
violation by some reasonable means, this is the first time you have
|
||||
received notice of violation of this License (for any work) from that
|
||||
copyright holder, and you cure the violation prior to 30 days after
|
||||
your receipt of the notice.
|
||||
|
||||
Termination of your rights under this section does not terminate the
|
||||
licenses of parties who have received copies or rights from you under
|
||||
this License. If your rights have been terminated and not permanently
|
||||
reinstated, you do not qualify to receive new licenses for the same
|
||||
material under section 10.
|
||||
|
||||
9. Acceptance Not Required for Having Copies.
|
||||
|
||||
You are not required to accept this License in order to receive or
|
||||
run a copy of the Program. Ancillary propagation of a covered work
|
||||
occurring solely as a consequence of using peer-to-peer transmission
|
||||
to receive a copy likewise does not require acceptance. However,
|
||||
nothing other than this License grants you permission to propagate or
|
||||
modify any covered work. These actions infringe copyright if you do
|
||||
not accept this License. Therefore, by modifying or propagating a
|
||||
covered work, you indicate your acceptance of this License to do so.
|
||||
|
||||
10. Automatic Licensing of Downstream Recipients.
|
||||
|
||||
Each time you convey a covered work, the recipient automatically
|
||||
receives a license from the original licensors, to run, modify and
|
||||
propagate that work, subject to this License. You are not responsible
|
||||
for enforcing compliance by third parties with this License.
|
||||
|
||||
An "entity transaction" is a transaction transferring control of an
|
||||
organization, or substantially all assets of one, or subdividing an
|
||||
organization, or merging organizations. If propagation of a covered
|
||||
work results from an entity transaction, each party to that
|
||||
transaction who receives a copy of the work also receives whatever
|
||||
licenses to the work the party's predecessor in interest had or could
|
||||
give under the previous paragraph, plus a right to possession of the
|
||||
Corresponding Source of the work from the predecessor in interest, if
|
||||
the predecessor has it or can get it with reasonable efforts.
|
||||
|
||||
You may not impose any further restrictions on the exercise of the
|
||||
rights granted or affirmed under this License. For example, you may
|
||||
not impose a license fee, royalty, or other charge for exercise of
|
||||
rights granted under this License, and you may not initiate litigation
|
||||
(including a cross-claim or counterclaim in a lawsuit) alleging that
|
||||
any patent claim is infringed by making, using, selling, offering for
|
||||
sale, or importing the Program or any portion of it.
|
||||
|
||||
11. Patents.
|
||||
|
||||
A "contributor" is a copyright holder who authorizes use under this
|
||||
License of the Program or a work on which the Program is based. The
|
||||
work thus licensed is called the contributor's "contributor version".
|
||||
|
||||
A contributor's "essential patent claims" are all patent claims
|
||||
owned or controlled by the contributor, whether already acquired or
|
||||
hereafter acquired, that would be infringed by some manner, permitted
|
||||
by this License, of making, using, or selling its contributor version,
|
||||
but do not include claims that would be infringed only as a
|
||||
consequence of further modification of the contributor version. For
|
||||
purposes of this definition, "control" includes the right to grant
|
||||
patent sublicenses in a manner consistent with the requirements of
|
||||
this License.
|
||||
|
||||
Each contributor grants you a non-exclusive, worldwide, royalty-free
|
||||
patent license under the contributor's essential patent claims, to
|
||||
make, use, sell, offer for sale, import and otherwise run, modify and
|
||||
propagate the contents of its contributor version.
|
||||
|
||||
In the following three paragraphs, a "patent license" is any express
|
||||
agreement or commitment, however denominated, not to enforce a patent
|
||||
(such as an express permission to practice a patent or covenant not to
|
||||
sue for patent infringement). To "grant" such a patent license to a
|
||||
party means to make such an agreement or commitment not to enforce a
|
||||
patent against the party.
|
||||
|
||||
If you convey a covered work, knowingly relying on a patent license,
|
||||
and the Corresponding Source of the work is not available for anyone
|
||||
to copy, free of charge and under the terms of this License, through a
|
||||
publicly available network server or other readily accessible means,
|
||||
then you must either (1) cause the Corresponding Source to be so
|
||||
available, or (2) arrange to deprive yourself of the benefit of the
|
||||
patent license for this particular work, or (3) arrange, in a manner
|
||||
consistent with the requirements of this License, to extend the patent
|
||||
license to downstream recipients. "Knowingly relying" means you have
|
||||
actual knowledge that, but for the patent license, your conveying the
|
||||
covered work in a country, or your recipient's use of the covered work
|
||||
in a country, would infringe one or more identifiable patents in that
|
||||
country that you have reason to believe are valid.
|
||||
|
||||
If, pursuant to or in connection with a single transaction or
|
||||
arrangement, you convey, or propagate by procuring conveyance of, a
|
||||
covered work, and grant a patent license to some of the parties
|
||||
receiving the covered work authorizing them to use, propagate, modify
|
||||
or convey a specific copy of the covered work, then the patent license
|
||||
you grant is automatically extended to all recipients of the covered
|
||||
work and works based on it.
|
||||
|
||||
A patent license is "discriminatory" if it does not include within
|
||||
the scope of its coverage, prohibits the exercise of, or is
|
||||
conditioned on the non-exercise of one or more of the rights that are
|
||||
specifically granted under this License. You may not convey a covered
|
||||
work if you are a party to an arrangement with a third party that is
|
||||
in the business of distributing software, under which you make payment
|
||||
to the third party based on the extent of your activity of conveying
|
||||
the work, and under which the third party grants, to any of the
|
||||
parties who would receive the covered work from you, a discriminatory
|
||||
patent license (a) in connection with copies of the covered work
|
||||
conveyed by you (or copies made from those copies), or (b) primarily
|
||||
for and in connection with specific products or compilations that
|
||||
contain the covered work, unless you entered into that arrangement,
|
||||
or that patent license was granted, prior to 28 March 2007.
|
||||
|
||||
Nothing in this License shall be construed as excluding or limiting
|
||||
any implied license or other defenses to infringement that may
|
||||
otherwise be available to you under applicable patent law.
|
||||
|
||||
12. No Surrender of Others' Freedom.
|
||||
|
||||
If conditions are imposed on you (whether by court order, agreement or
|
||||
otherwise) that contradict the conditions of this License, they do not
|
||||
excuse you from the conditions of this License. If you cannot convey a
|
||||
covered work so as to satisfy simultaneously your obligations under this
|
||||
License and any other pertinent obligations, then as a consequence you may
|
||||
not convey it at all. For example, if you agree to terms that obligate you
|
||||
to collect a royalty for further conveying from those to whom you convey
|
||||
the Program, the only way you could satisfy both those terms and this
|
||||
License would be to refrain entirely from conveying the Program.
|
||||
|
||||
13. Use with the GNU Affero General Public License.
|
||||
|
||||
Notwithstanding any other provision of this License, you have
|
||||
permission to link or combine any covered work with a work licensed
|
||||
under version 3 of the GNU Affero General Public License into a single
|
||||
combined work, and to convey the resulting work. The terms of this
|
||||
License will continue to apply to the part which is the covered work,
|
||||
but the special requirements of the GNU Affero General Public License,
|
||||
section 13, concerning interaction through a network will apply to the
|
||||
combination as such.
|
||||
|
||||
14. Revised Versions of this License.
|
||||
|
||||
The Free Software Foundation may publish revised and/or new versions of
|
||||
the GNU General Public License from time to time. Such new versions will
|
||||
be similar in spirit to the present version, but may differ in detail to
|
||||
address new problems or concerns.
|
||||
|
||||
Each version is given a distinguishing version number. If the
|
||||
Program specifies that a certain numbered version of the GNU General
|
||||
Public License "or any later version" applies to it, you have the
|
||||
option of following the terms and conditions either of that numbered
|
||||
version or of any later version published by the Free Software
|
||||
Foundation. If the Program does not specify a version number of the
|
||||
GNU General Public License, you may choose any version ever published
|
||||
by the Free Software Foundation.
|
||||
|
||||
If the Program specifies that a proxy can decide which future
|
||||
versions of the GNU General Public License can be used, that proxy's
|
||||
public statement of acceptance of a version permanently authorizes you
|
||||
to choose that version for the Program.
|
||||
|
||||
Later license versions may give you additional or different
|
||||
permissions. However, no additional obligations are imposed on any
|
||||
author or copyright holder as a result of your choosing to follow a
|
||||
later version.
|
||||
|
||||
15. Disclaimer of Warranty.
|
||||
|
||||
THERE IS NO WARRANTY FOR THE PROGRAM, TO THE EXTENT PERMITTED BY
|
||||
APPLICABLE LAW. EXCEPT WHEN OTHERWISE STATED IN WRITING THE COPYRIGHT
|
||||
HOLDERS AND/OR OTHER PARTIES PROVIDE THE PROGRAM "AS IS" WITHOUT WARRANTY
|
||||
OF ANY KIND, EITHER EXPRESSED OR IMPLIED, INCLUDING, BUT NOT LIMITED TO,
|
||||
THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR
|
||||
PURPOSE. THE ENTIRE RISK AS TO THE QUALITY AND PERFORMANCE OF THE PROGRAM
|
||||
IS WITH YOU. SHOULD THE PROGRAM PROVE DEFECTIVE, YOU ASSUME THE COST OF
|
||||
ALL NECESSARY SERVICING, REPAIR OR CORRECTION.
|
||||
|
||||
16. Limitation of Liability.
|
||||
|
||||
IN NO EVENT UNLESS REQUIRED BY APPLICABLE LAW OR AGREED TO IN WRITING
|
||||
WILL ANY COPYRIGHT HOLDER, OR ANY OTHER PARTY WHO MODIFIES AND/OR CONVEYS
|
||||
THE PROGRAM AS PERMITTED ABOVE, BE LIABLE TO YOU FOR DAMAGES, INCLUDING ANY
|
||||
GENERAL, SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES ARISING OUT OF THE
|
||||
USE OR INABILITY TO USE THE PROGRAM (INCLUDING BUT NOT LIMITED TO LOSS OF
|
||||
DATA OR DATA BEING RENDERED INACCURATE OR LOSSES SUSTAINED BY YOU OR THIRD
|
||||
PARTIES OR A FAILURE OF THE PROGRAM TO OPERATE WITH ANY OTHER PROGRAMS),
|
||||
EVEN IF SUCH HOLDER OR OTHER PARTY HAS BEEN ADVISED OF THE POSSIBILITY OF
|
||||
SUCH DAMAGES.
|
||||
|
||||
17. Interpretation of Sections 15 and 16.
|
||||
|
||||
If the disclaimer of warranty and limitation of liability provided
|
||||
above cannot be given local legal effect according to their terms,
|
||||
reviewing courts shall apply local law that most closely approximates
|
||||
an absolute waiver of all civil liability in connection with the
|
||||
Program, unless a warranty or assumption of liability accompanies a
|
||||
copy of the Program in return for a fee.
|
||||
|
||||
END OF TERMS AND CONDITIONS
|
||||
|
||||
How to Apply These Terms to Your New Programs
|
||||
|
||||
If you develop a new program, and you want it to be of the greatest
|
||||
possible use to the public, the best way to achieve this is to make it
|
||||
free software which everyone can redistribute and change under these terms.
|
||||
|
||||
To do so, attach the following notices to the program. It is safest
|
||||
to attach them to the start of each source file to most effectively
|
||||
state the exclusion of warranty; and each file should have at least
|
||||
the "copyright" line and a pointer to where the full notice is found.
|
||||
|
||||
<one line to give the program's name and a brief idea of what it does.>
|
||||
Copyright (C) <year> <name of author>
|
||||
|
||||
This program is free software: you can redistribute it and/or modify
|
||||
it under the terms of the GNU General Public License as published by
|
||||
the Free Software Foundation, either version 3 of the License, or
|
||||
(at your option) any later version.
|
||||
|
||||
This program is distributed in the hope that it will be useful,
|
||||
but WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
|
||||
GNU General Public License for more details.
|
||||
|
||||
You should have received a copy of the GNU General Public License
|
||||
along with this program. If not, see <http://www.gnu.org/licenses/>.
|
||||
|
||||
Also add information on how to contact you by electronic and paper mail.
|
||||
|
||||
If the program does terminal interaction, make it output a short
|
||||
notice like this when it starts in an interactive mode:
|
||||
|
||||
<program> Copyright (C) <year> <name of author>
|
||||
This program comes with ABSOLUTELY NO WARRANTY; for details type `show w'.
|
||||
This is free software, and you are welcome to redistribute it
|
||||
under certain conditions; type `show c' for details.
|
||||
|
||||
The hypothetical commands `show w' and `show c' should show the appropriate
|
||||
parts of the General Public License. Of course, your program's commands
|
||||
might be different; for a GUI interface, you would use an "about box".
|
||||
|
||||
You should also get your employer (if you work as a programmer) or school,
|
||||
if any, to sign a "copyright disclaimer" for the program, if necessary.
|
||||
For more information on this, and how to apply and follow the GNU GPL, see
|
||||
<http://www.gnu.org/licenses/>.
|
||||
|
||||
The GNU General Public License does not permit incorporating your program
|
||||
into proprietary programs. If your program is a subroutine library, you
|
||||
may consider it more useful to permit linking proprietary applications with
|
||||
the library. If this is what you want to do, use the GNU Lesser General
|
||||
Public License instead of this License. But first, please read
|
||||
<http://www.gnu.org/philosophy/why-not-lgpl.html>.
|
||||
|
||||
20
README.TXT
Normal file
20
README.TXT
Normal file
@ -0,0 +1,20 @@
|
||||
|
||||
OpenRocket - an Open Source model rocket simulator
|
||||
--------------------------------------------------
|
||||
|
||||
Copyright (C) 2007-2009 Sampo Niskanen
|
||||
|
||||
|
||||
For license information see the file LICENSE.TXT.
|
||||
|
||||
For more information see http://openrocket.sourceforge.net/
|
||||
|
||||
|
||||
|
||||
To start the software run the class
|
||||
|
||||
net.sf.openrocket.gui.main.BasicFrame
|
||||
|
||||
or from the JAR file run
|
||||
|
||||
$ java -jar OpenRocket-<VERSION>.jar
|
||||
126
TODO
Normal file
126
TODO
Normal file
@ -0,0 +1,126 @@
|
||||
|
||||
GUI:
|
||||
|
||||
- Preferences dialog
|
||||
|
||||
|
||||
BUGS:
|
||||
|
||||
|
||||
COMPUTATION:
|
||||
|
||||
|
||||
FILE/STORAGE:
|
||||
|
||||
|
||||
OTHER:
|
||||
|
||||
- web-sivut
|
||||
|
||||
|
||||
DIPPA:
|
||||
|
||||
|
||||
|
||||
|
||||
-------------------
|
||||
|
||||
LATER:
|
||||
|
||||
- Simulation delete/copy/paste hotkeys
|
||||
(either component or simulation selected, but not both)
|
||||
- Add BodyComponent at end of rocket when no component is selected
|
||||
- Showing events in plot (maybe future)
|
||||
- Search field in motor selection dialog
|
||||
- Through-the-wall fins
|
||||
- Store materials
|
||||
|
||||
- Streamer CD estimation
|
||||
|
||||
- exporting (maybe later)
|
||||
|
||||
- Make ThicknessRingComponent implement RadialParent and allow
|
||||
attaching components to a TubeCoupler
|
||||
|
||||
|
||||
|
||||
|
||||
DONE:
|
||||
|
||||
- Automatic diameters of body components
|
||||
- Copy/paste
|
||||
|
||||
18.4.:
|
||||
- Esc, Ctrl-Z and Y etc.
|
||||
- Look and feel
|
||||
|
||||
19.4.:
|
||||
- Nose cone and transition shoulders in GUI
|
||||
- zoom, cut/copy/paste etc. icons
|
||||
|
||||
23.4.:
|
||||
- Figure or rocket not updating when using a new BasicFrame
|
||||
|
||||
24.4.:
|
||||
- File save and load
|
||||
- Motor configuration editing (pre-alpha)
|
||||
- Save simulations
|
||||
|
||||
25.4.:
|
||||
- Multi-stages simulation (pre-alpha)
|
||||
- Make sure simulations end
|
||||
- Mass and CG overrides (pre-alpha)
|
||||
- General loader
|
||||
|
||||
26.4.:
|
||||
- Centering ring inner diameter automatics (pre-alpha)
|
||||
- Landing simulation (pre-alpha ??)
|
||||
- Parachute/Streamer editing in GUI (pre-alpha)
|
||||
- Launch lug editing in GUI (pre-alpha)
|
||||
|
||||
29.4.:
|
||||
- Actual plotting done
|
||||
- Refactored source code packages
|
||||
|
||||
2.5.:
|
||||
- Plotting (pre-alpha)
|
||||
- Gravity model
|
||||
- More units and specific custom units (angle, temperature, ...)
|
||||
- Transition/Nose cone description text wrapping
|
||||
- Fin set CP jumps at Mach 0.9
|
||||
|
||||
- Error dialogs for load/save/etc
|
||||
|
||||
3.5.:
|
||||
- More materials (pre-alpha)
|
||||
- File opening from command line
|
||||
|
||||
9.5.:
|
||||
- Rocket configuration dialog
|
||||
- Warnings in poor conditions (transition supersonic)
|
||||
- New or old fin-body interference?
|
||||
- poista tiedot laminaarisesta vastuksesta
|
||||
- vertailuosio
|
||||
|
||||
11.5.:
|
||||
- Better default values for components
|
||||
- Component analysis dialog show zero total mass and CG
|
||||
- Compression support in save
|
||||
- Simulation storage options
|
||||
|
||||
12.5.:
|
||||
- Load simulations
|
||||
- Update file version to 1.0
|
||||
|
||||
13.5.:
|
||||
- statistiikat softasta
|
||||
|
||||
17.5.:
|
||||
- jonkin verran TODOja
|
||||
- conclusion
|
||||
- viitteet
|
||||
- Draw the component icons
|
||||
- splashscreen
|
||||
|
||||
18.5.:
|
||||
- About dialog + version number
|
||||
63
build.xml
Normal file
63
build.xml
Normal file
@ -0,0 +1,63 @@
|
||||
<project name="OpenRocket" basedir=".">
|
||||
|
||||
<property name="src.dir" value="src"/> <!-- Source directory -->
|
||||
<property name="build.dir" value="build"/> <!-- Build directory -->
|
||||
|
||||
<!-- Distribution directory, from which stuff is jar'ed -->
|
||||
<property name="dist.dir" value="${build.dir}/dist"/>
|
||||
|
||||
<property name="classes.dir" value="${dist.dir}"/> <!-- Directory for classes -->
|
||||
<property name="jar.dir" value="${build.dir}/jar"/> <!-- Directory for built jar's -->
|
||||
<property name="lib.dir" value="lib"/> <!-- Library source directory -->
|
||||
|
||||
|
||||
<!-- The main class of the application -->
|
||||
<property name="main-class" value="net.sf.openrocket.gui.main.BasicFrame"/>
|
||||
|
||||
|
||||
<!-- Classpath definition -->
|
||||
<path id="classpath">
|
||||
<fileset dir="${lib.dir}" includes="**/*.jar"/>
|
||||
</path>
|
||||
|
||||
|
||||
<!-- CLEAN -->
|
||||
<target name="clean">
|
||||
<delete dir="${build.dir}"/>
|
||||
</target>
|
||||
|
||||
<!-- BUILD -->
|
||||
<target name="build">
|
||||
<mkdir dir="${classes.dir}"/>
|
||||
<javac srcdir="${src.dir}" destdir="${classes.dir}" classpathref="classpath"/>
|
||||
</target>
|
||||
|
||||
<!-- JAR -->
|
||||
<target name="jar" depends="build">
|
||||
<copy todir="${dist.dir}/">
|
||||
<fileset dir="." includes="LICENSE.TXT" />
|
||||
<fileset dir="." includes="README.TXT" />
|
||||
<fileset dir="." includes="datafiles/**/* pix/**/*" />
|
||||
</copy>
|
||||
<mkdir dir="${jar.dir}"/>
|
||||
<jar destfile="${jar.dir}/${ant.project.name}.jar" basedir="${dist.dir}">
|
||||
<manifest>
|
||||
<attribute name="Main-Class" value="${main-class}"/>
|
||||
<attribute name="SplashScreen-Image" value="pix/splashscreen.png"/>
|
||||
</manifest>
|
||||
<zipfileset src="lib/miglayout15-swing.jar" />
|
||||
<zipfileset src="lib/jcommon-1.0.16.jar" />
|
||||
<zipfileset src="lib/jfreechart-1.0.13.jar" />
|
||||
</jar>
|
||||
</target>
|
||||
|
||||
<!-- RUN -->
|
||||
<target name="run" depends="jar">
|
||||
<java fork="true" classname="${main-class}">
|
||||
<classpath>
|
||||
<path location="${jar.dir}/${ant.project.name}.jar"/>
|
||||
</classpath>
|
||||
</java>
|
||||
</target>
|
||||
|
||||
</project>
|
||||
3685
datafiles/thrustcurves/00INDEX.txt
Normal file
3685
datafiles/thrustcurves/00INDEX.txt
Normal file
File diff suppressed because it is too large
Load Diff
33
datafiles/thrustcurves/AMW_I195.eng
Normal file
33
datafiles/thrustcurves/AMW_I195.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;Animal Motor Works 38-390
|
||||
I195WT 38 249 17 0.193 0.495 AMW
|
||||
0.0020 10.548
|
||||
0.018 42.653
|
||||
0.046 136.214
|
||||
0.064 179.784
|
||||
0.072 191.248
|
||||
0.078 197.211
|
||||
0.088 198.587
|
||||
0.126 198.587
|
||||
0.175 207.759
|
||||
0.217 211.887
|
||||
0.349 216.931
|
||||
0.401 221.059
|
||||
0.554 225.646
|
||||
0.586 228.856
|
||||
0.626 228.48
|
||||
0.65 230.232
|
||||
1.013 231.607
|
||||
1.105 230.691
|
||||
1.2 225.187
|
||||
1.356 210.511
|
||||
1.392 207.759
|
||||
1.441 206.842
|
||||
1.457 205.007
|
||||
1.519 181.159
|
||||
1.563 155.936
|
||||
1.693 49.992
|
||||
1.727 28.435
|
||||
1.756 16.512
|
||||
1.798 7.338
|
||||
1.86 1.376
|
||||
1.89 0.0
|
||||
29
datafiles/thrustcurves/AMW_I220.eng
Normal file
29
datafiles/thrustcurves/AMW_I220.eng
Normal file
@ -0,0 +1,29 @@
|
||||
;Animal Motor Works 38-390
|
||||
I220SK 38 249 20 0.202 0.495 AMW
|
||||
0.0050 12.747
|
||||
0.019 45.25
|
||||
0.036 79.666
|
||||
0.052 125.554
|
||||
0.069 162.519
|
||||
0.076 169.53
|
||||
0.095 174.629
|
||||
0.167 176.541
|
||||
0.229 191.199
|
||||
0.447 235.175
|
||||
0.602 260.668
|
||||
0.733 288.073
|
||||
0.85 302.095
|
||||
0.974 301.457
|
||||
1.094 289.985
|
||||
1.184 268.954
|
||||
1.268 240.273
|
||||
1.302 219.879
|
||||
1.388 177.178
|
||||
1.418 147.224
|
||||
1.435 127.467
|
||||
1.473 91.139
|
||||
1.504 65.645
|
||||
1.543 40.789
|
||||
1.593 19.12
|
||||
1.622 10.197
|
||||
1.65 0.0
|
||||
27
datafiles/thrustcurves/AMW_I271.eng
Normal file
27
datafiles/thrustcurves/AMW_I271.eng
Normal file
@ -0,0 +1,27 @@
|
||||
;
|
||||
; AMW 38-390
|
||||
I271BB 38 258 0 0.189 0.493 AMW
|
||||
0.011 119.530
|
||||
0.035 213.907
|
||||
0.050 245.903
|
||||
0.074 262.705
|
||||
0.115 269.446
|
||||
0.225 267.736
|
||||
0.346 282.929
|
||||
0.465 296.411
|
||||
0.584 303.152
|
||||
0.727 311.504
|
||||
0.916 318.245
|
||||
1.054 324.986
|
||||
1.162 331.400
|
||||
1.201 326.696
|
||||
1.225 313.214
|
||||
1.242 286.249
|
||||
1.268 240.990
|
||||
1.294 188.888
|
||||
1.323 136.833
|
||||
1.346 87.565
|
||||
1.368 45.467
|
||||
1.392 18.523
|
||||
1.430 0.000
|
||||
;
|
||||
31
datafiles/thrustcurves/AMW_I285.eng
Normal file
31
datafiles/thrustcurves/AMW_I285.eng
Normal file
@ -0,0 +1,31 @@
|
||||
;
|
||||
; AMW 38-390
|
||||
I285GG 38 258 0 0.206 0.515 AMW
|
||||
0.013 61.575
|
||||
0.032 119.327
|
||||
0.055 164.575
|
||||
0.076 191.004
|
||||
0.094 201.014
|
||||
0.139 212.326
|
||||
0.232 231.247
|
||||
0.357 258.876
|
||||
0.456 267.686
|
||||
0.592 278.998
|
||||
0.716 289.358
|
||||
0.841 291.200
|
||||
0.936 290.310
|
||||
1.051 285.204
|
||||
1.139 277.696
|
||||
1.204 280.199
|
||||
1.243 278.998
|
||||
1.265 268.887
|
||||
1.286 242.559
|
||||
1.319 187.200
|
||||
1.359 134.443
|
||||
1.387 86.702
|
||||
1.407 52.776
|
||||
1.428 31.413
|
||||
1.448 16.337
|
||||
1.465 5.026
|
||||
1.480 0.000
|
||||
;
|
||||
34
datafiles/thrustcurves/AMW_I315.eng
Normal file
34
datafiles/thrustcurves/AMW_I315.eng
Normal file
@ -0,0 +1,34 @@
|
||||
; This file my be used or given away. All I ask is that this header
|
||||
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
;Animal Motor Works 38-640
|
||||
I315SK 38 369 20 0.3829 0.7166 AMW
|
||||
0.011 314.573
|
||||
0.030 312.796
|
||||
0.066 300.786
|
||||
0.084 300.502
|
||||
0.120 304.087
|
||||
0.175 312.998
|
||||
0.266 324.086
|
||||
0.356 332.224
|
||||
0.447 347.855
|
||||
0.538 371.972
|
||||
0.629 382.833
|
||||
0.719 385.552
|
||||
0.810 385.586
|
||||
0.901 384.836
|
||||
0.992 382.296
|
||||
1.082 378.323
|
||||
1.173 370.837
|
||||
1.264 357.564
|
||||
1.355 347.122
|
||||
1.445 328.332
|
||||
1.536 202.733
|
||||
1.627 90.867
|
||||
1.718 35.427
|
||||
1.808 8.192
|
||||
1.815 0.000
|
||||
31
datafiles/thrustcurves/AMW_I325.eng
Normal file
31
datafiles/thrustcurves/AMW_I325.eng
Normal file
@ -0,0 +1,31 @@
|
||||
;Animal Motor Works 38-640
|
||||
I325WT 38 370 17 0.317 0.712 AMW
|
||||
0.014 68.710
|
||||
0.022 113.038
|
||||
0.026 153.671
|
||||
0.037 244.545
|
||||
0.045 299.216
|
||||
0.055 330.246
|
||||
0.065 350.194
|
||||
0.079 365.709
|
||||
0.094 376.79
|
||||
0.124 381.963
|
||||
0.185 373.836
|
||||
0.252 373.836
|
||||
0.35 381.224
|
||||
0.47 382.701
|
||||
0.622 388.611
|
||||
1.102 384.179
|
||||
1.366 364.971
|
||||
1.379 360.537
|
||||
1.415 331.724
|
||||
1.49 223.119
|
||||
1.505 211.298
|
||||
1.551 187.657
|
||||
1.592 162.538
|
||||
1.688 80.529
|
||||
1.726 50.978
|
||||
1.775 27.336
|
||||
1.806 16.993
|
||||
1.834 9.605
|
||||
1.901 0.0
|
||||
26
datafiles/thrustcurves/AMW_I375.eng
Normal file
26
datafiles/thrustcurves/AMW_I375.eng
Normal file
@ -0,0 +1,26 @@
|
||||
;
|
||||
;Animal Motor Works 38-640
|
||||
I375GG 38 369 20 0.3936 0.7338 AMW
|
||||
0.013 223.878
|
||||
0.045 273.929
|
||||
0.092 312.421
|
||||
0.140 334.383
|
||||
0.219 357.983
|
||||
0.298 381.992
|
||||
0.377 410.267
|
||||
0.457 431.141
|
||||
0.536 454.458
|
||||
0.615 476.825
|
||||
0.694 495.473
|
||||
0.773 504.665
|
||||
0.852 510.942
|
||||
0.931 511.972
|
||||
1.011 489.639
|
||||
1.090 441.350
|
||||
1.169 392.762
|
||||
1.248 354.753
|
||||
1.327 292.385
|
||||
1.406 177.309
|
||||
1.486 63.879
|
||||
1.565 14.901
|
||||
1.583 0.000
|
||||
35
datafiles/thrustcurves/AMW_J357.eng
Normal file
35
datafiles/thrustcurves/AMW_J357.eng
Normal file
@ -0,0 +1,35 @@
|
||||
; AMW Animal Motor Works fixed by dberez 12/08/03
|
||||
;
|
||||
;Animal Motor Works J357 White Wolf
|
||||
J357WW 54 326 0 0.5481 1.2101 AMW
|
||||
0.02 129.64
|
||||
0.03 205.95
|
||||
0.05 265.00
|
||||
0.06 316.51
|
||||
0.09 326.05
|
||||
0.13 314.60
|
||||
0.18 301.25
|
||||
0.24 299.34
|
||||
0.35 312.69
|
||||
0.50 326.05
|
||||
0.66 333.68
|
||||
0.87 345.13
|
||||
1.07 358.48
|
||||
1.46 383.18
|
||||
1.77 398.45
|
||||
1.86 400.36
|
||||
1.98 402.35
|
||||
2.18 398.45
|
||||
2.29 390.82
|
||||
2.41 369.93
|
||||
2.51 354.67
|
||||
2.55 352.76
|
||||
2.60 347.03
|
||||
2.65 335.59
|
||||
2.69 310.79
|
||||
2.75 249.73
|
||||
2.81 175.43
|
||||
2.84 108.65
|
||||
2.90 53.38
|
||||
2.92 20.98
|
||||
2.95 0.00
|
||||
25
datafiles/thrustcurves/AMW_J365.eng
Normal file
25
datafiles/thrustcurves/AMW_J365.eng
Normal file
@ -0,0 +1,25 @@
|
||||
;
|
||||
;Animal Motor Works 54-1400
|
||||
J365SK 54 403 0 0.7571 1.4593 AMW
|
||||
0.029 389.731
|
||||
0.123 360.219
|
||||
0.218 334.200
|
||||
0.376 326.150
|
||||
0.534 334.217
|
||||
0.692 341.669
|
||||
0.850 347.676
|
||||
1.007 359.408
|
||||
1.165 370.043
|
||||
1.323 383.343
|
||||
1.481 399.248
|
||||
1.639 417.477
|
||||
1.797 443.735
|
||||
1.955 472.683
|
||||
2.112 501.668
|
||||
2.270 497.077
|
||||
2.428 425.371
|
||||
2.586 349.017
|
||||
2.744 262.068
|
||||
2.902 107.073
|
||||
3.060 41.821
|
||||
3.157 0.000
|
||||
44
datafiles/thrustcurves/AMW_J370.eng
Normal file
44
datafiles/thrustcurves/AMW_J370.eng
Normal file
@ -0,0 +1,44 @@
|
||||
;
|
||||
;Animal Motor Works 54-1050
|
||||
;AMW J370GG RASP.ENG file made from NAR data
|
||||
;File produced FEB 20, 2003
|
||||
;This file my be used or given away. All I ask is that this header
|
||||
;is maintained to give credit to NAR S&T. Thank you, Jack Kane
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
J370GG 54 326 100 0.5983 1.2491 Animal_Motor_Works
|
||||
0.008 185.496
|
||||
0.024 149.516
|
||||
0.063 225.273
|
||||
0.087 272.647
|
||||
0.122 304.829
|
||||
0.158 304.829
|
||||
0.273 335.212
|
||||
0.431 363.796
|
||||
0.573 390.381
|
||||
0.707 413.168
|
||||
0.877 428.459
|
||||
1.019 441.852
|
||||
1.126 441.852
|
||||
1.224 458.46
|
||||
1.284 443.951
|
||||
1.386 440.153
|
||||
1.572 438.454
|
||||
1.651 438.554
|
||||
1.813 417.765
|
||||
2.022 404.673
|
||||
2.141 385.883
|
||||
2.212 385.883
|
||||
2.255 374.59
|
||||
2.299 387.882
|
||||
2.362 357.599
|
||||
2.401 384.184
|
||||
2.421 348.204
|
||||
2.457 316.122
|
||||
2.559 251.758
|
||||
2.697 115.635
|
||||
2.753 45.624
|
||||
2.82 0
|
||||
34
datafiles/thrustcurves/AMW_J400.eng
Normal file
34
datafiles/thrustcurves/AMW_J400.eng
Normal file
@ -0,0 +1,34 @@
|
||||
;
|
||||
;AMW J400 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
J400RR 54 326 100 0.558 1.2314 Animal_Motor_Works
|
||||
0.043 246.55
|
||||
0.06 317.381
|
||||
0.081 344.709
|
||||
0.107 358.372
|
||||
0.15 356.06
|
||||
0.201 365.204
|
||||
0.308 392.532
|
||||
0.568 435.734
|
||||
0.863 458.339
|
||||
1.094 469.24
|
||||
1.209 467.18
|
||||
1.466 460.148
|
||||
1.705 443.972
|
||||
1.923 423.275
|
||||
2.132 409.411
|
||||
2.303 413.831
|
||||
2.402 420.563
|
||||
2.47 413.831
|
||||
2.517 395.445
|
||||
2.543 347.421
|
||||
2.568 265.238
|
||||
2.598 128.198
|
||||
2.615 68.801
|
||||
2.632 25.398
|
||||
2.66 0
|
||||
27
datafiles/thrustcurves/AMW_J440.eng
Normal file
27
datafiles/thrustcurves/AMW_J440.eng
Normal file
@ -0,0 +1,27 @@
|
||||
;Animal Motor Works 38-640
|
||||
J440BB 38 369 20 0.3853 0.6985 AMW
|
||||
0.007 468.505
|
||||
0.022 509.996
|
||||
0.037 527.687
|
||||
0.052 532.792
|
||||
0.082 530.181
|
||||
0.127 525.586
|
||||
0.202 521.566
|
||||
0.277 519.840
|
||||
0.352 521.522
|
||||
0.426 525.414
|
||||
0.501 531.248
|
||||
0.576 538.724
|
||||
0.651 541.761
|
||||
0.726 538.508
|
||||
0.801 531.072
|
||||
0.876 516.175
|
||||
0.950 494.942
|
||||
1.025 477.251
|
||||
1.100 433.297
|
||||
1.175 313.900
|
||||
1.250 187.467
|
||||
1.325 101.546
|
||||
1.400 45.751
|
||||
1.474 22.083
|
||||
1.497 0.000
|
||||
39
datafiles/thrustcurves/AMW_J450.eng
Normal file
39
datafiles/thrustcurves/AMW_J450.eng
Normal file
@ -0,0 +1,39 @@
|
||||
;
|
||||
;AMW J450 RASP.ENG file made from NAR published data
|
||||
; File produced SEPT 4, 2002
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
J450 54 326 P .5331 1.1964 AMW
|
||||
0.009 251.586
|
||||
0.016 376.074
|
||||
0.030 413.450
|
||||
0.051 430.832
|
||||
0.094 423.296
|
||||
0.162 413.149
|
||||
0.262 395.566
|
||||
0.402 420.182
|
||||
0.495 444.898
|
||||
0.805 504.078
|
||||
1.048 536.028
|
||||
1.223 550.597
|
||||
1.299 563.180
|
||||
1.334 555.319
|
||||
1.470 560.042
|
||||
1.588 559.841
|
||||
1.764 546.980
|
||||
1.921 516.838
|
||||
1.993 496.743
|
||||
2.025 499.154
|
||||
2.047 479.160
|
||||
2.086 414.354
|
||||
2.115 344.525
|
||||
2.141 252.290
|
||||
2.177 140.161
|
||||
2.213 82.780
|
||||
2.239 50.347
|
||||
2.271 27.861
|
||||
2.296 12.860
|
||||
2.330 0.000
|
||||
33
datafiles/thrustcurves/AMW_J450_1.eng
Normal file
33
datafiles/thrustcurves/AMW_J450_1.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;
|
||||
;Animal Motor Works J450 Super Tiger
|
||||
J450ST 54 326 0 0.5331 1.1964 AMW
|
||||
0.009 251.586
|
||||
0.016 376.074
|
||||
0.030 413.450
|
||||
0.051 430.832
|
||||
0.094 423.296
|
||||
0.162 413.149
|
||||
0.262 395.566
|
||||
0.402 420.182
|
||||
0.495 444.898
|
||||
0.805 504.078
|
||||
1.048 536.028
|
||||
1.223 550.597
|
||||
1.299 563.180
|
||||
1.334 555.319
|
||||
1.470 560.042
|
||||
1.588 559.841
|
||||
1.764 546.980
|
||||
1.921 516.838
|
||||
1.993 496.743
|
||||
2.025 499.154
|
||||
2.047 479.160
|
||||
2.086 414.354
|
||||
2.115 344.525
|
||||
2.141 252.290
|
||||
2.177 140.161
|
||||
2.213 82.780
|
||||
2.239 50.347
|
||||
2.271 27.861
|
||||
2.296 12.860
|
||||
2.330 0.000
|
||||
32
datafiles/thrustcurves/AMW_J480.eng
Normal file
32
datafiles/thrustcurves/AMW_J480.eng
Normal file
@ -0,0 +1,32 @@
|
||||
;
|
||||
;AMW J480 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
J480BB 54 326 100 0.556 1.2131 Animal_Motor_Works
|
||||
0.015 225.429
|
||||
0.041 348.18
|
||||
0.071 388.127
|
||||
0.194 422.453
|
||||
0.385 459.49
|
||||
0.699 502.347
|
||||
0.968 528.042
|
||||
1.2 536.573
|
||||
1.454 543.15
|
||||
1.674 533.763
|
||||
1.887 522.321
|
||||
2.044 519.41
|
||||
2.108 525.131
|
||||
2.164 528.042
|
||||
2.197 488.095
|
||||
2.25 419.543
|
||||
2.283 333.928
|
||||
2.328 231.15
|
||||
2.354 176.95
|
||||
2.392 111.309
|
||||
2.418 68.501
|
||||
2.436 37.106
|
||||
2.49 0
|
||||
32
datafiles/thrustcurves/AMW_J500.eng
Normal file
32
datafiles/thrustcurves/AMW_J500.eng
Normal file
@ -0,0 +1,32 @@
|
||||
;
|
||||
;J500ST entered by Tim Van Milligan
|
||||
;For RockSim - http://www.rocksim.com
|
||||
;Based on TRA Certification paperwork from 06-01-2002
|
||||
;Initial Mass from Jim Robinson at AMW
|
||||
;Not approved by TRA or AMW.
|
||||
J500ST 38 370 20 0.3265 0.744 Animal_Motor_Works
|
||||
0.006 444.822
|
||||
0.025 475.651
|
||||
0.04 418.397
|
||||
0.053 466.843
|
||||
0.059 409.589
|
||||
0.071 458.035
|
||||
0.077 409.589
|
||||
0.1 444.822
|
||||
0.127 506.481
|
||||
0.204 590.16
|
||||
0.25 644.992
|
||||
0.3 678.244
|
||||
0.34 709.073
|
||||
0.402 735.498
|
||||
0.445 766.327
|
||||
0.516 783.944
|
||||
0.6 787.335
|
||||
0.637 770.732
|
||||
0.68 744.306
|
||||
0.76 620.989
|
||||
0.859 475.651
|
||||
1.00464 303.888
|
||||
1.122 171.763
|
||||
1.227 52.8502
|
||||
1.3 0
|
||||
37
datafiles/thrustcurves/AMW_K1000.eng
Normal file
37
datafiles/thrustcurves/AMW_K1000.eng
Normal file
@ -0,0 +1,37 @@
|
||||
;
|
||||
;AMW K1000 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K1000SK 54 728 100 1.297 2.556 Animal_Motor_Works
|
||||
0.019 1155.06
|
||||
0.045 1426.12
|
||||
0.094 1248.23
|
||||
0.161 1112.99
|
||||
0.239 1128.02
|
||||
0.343 1113.99
|
||||
0.377 1149.05
|
||||
0.44 1121
|
||||
0.544 1221.18
|
||||
0.633 1178.11
|
||||
0.674 1221.18
|
||||
0.737 1193.13
|
||||
0.883 1200.14
|
||||
1.009 1194.13
|
||||
1.057 1236.21
|
||||
1.188 1137.03
|
||||
1.299 1145.05
|
||||
1.396 1087.94
|
||||
1.516 954.104
|
||||
1.631 855.228
|
||||
1.717 827.077
|
||||
1.777 650.061
|
||||
1.848 465.932
|
||||
1.93 303.141
|
||||
2.023 147.463
|
||||
2.083 83.879
|
||||
2.132 41.484
|
||||
2.18 0
|
||||
39
datafiles/thrustcurves/AMW_K1075.eng
Normal file
39
datafiles/thrustcurves/AMW_K1075.eng
Normal file
@ -0,0 +1,39 @@
|
||||
;
|
||||
;Animal Motor Works K1075 RASP.ENG file made from NAR data
|
||||
;File produced Feb 22, 2003
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K1075GG 54 726 100 1.3999 2.6658 Animal_Motor_Works
|
||||
0.009 672.664
|
||||
0.015 963.511
|
||||
0.022 860.518
|
||||
0.047 987.857
|
||||
0.075 975.835
|
||||
0.106 921.332
|
||||
0.215 958.001
|
||||
0.529 1092.05
|
||||
0.878 1220.29
|
||||
1.077 1269.39
|
||||
1.158 1311.47
|
||||
1.235 1293.43
|
||||
1.448 1330.5
|
||||
1.577 1318.48
|
||||
1.672 1319.48
|
||||
1.721 1337.52
|
||||
1.759 1337.52
|
||||
1.805 1337.52
|
||||
1.829 1331.5
|
||||
1.856 1384.67
|
||||
1.889 1277.4
|
||||
1.906 1216.29
|
||||
1.938 1052.98
|
||||
1.96 871.338
|
||||
1.988 659.239
|
||||
2.027 453.352
|
||||
2.062 301.967
|
||||
2.115 138.46
|
||||
2.168 41.608
|
||||
2.2 0
|
||||
35
datafiles/thrustcurves/AMW_K365.eng
Normal file
35
datafiles/thrustcurves/AMW_K365.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;AMW K365RR RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K365RR 75 111 100 0.946 2.3456 Animal_Motor_Works
|
||||
0.049 138.157
|
||||
0.068 381.241
|
||||
0.084 454.75
|
||||
0.106 481.536
|
||||
0.164 488.182
|
||||
0.291 514.867
|
||||
0.435 545.982
|
||||
0.666 561.49
|
||||
0.868 565.73
|
||||
1.082 565.518
|
||||
1.296 550.111
|
||||
1.591 529.871
|
||||
1.805 509.731
|
||||
1.828 536.517
|
||||
1.886 498.554
|
||||
2.124 467.237
|
||||
2.501 411.35
|
||||
2.924 328.677
|
||||
3.296 241.573
|
||||
3.638 172.293
|
||||
3.969 100.798
|
||||
4.195 56.098
|
||||
4.265 51.607
|
||||
4.346 35.959
|
||||
4.433 15.859
|
||||
4.51 0
|
||||
35
datafiles/thrustcurves/AMW_K450.eng
Normal file
35
datafiles/thrustcurves/AMW_K450.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;AMW K450BB RASP.ENG file made from NAR published data
|
||||
;File produced Aug 19, 2003
|
||||
;This file my be used or given away. All I ask is that this header
|
||||
;is maintained to give credit to NAR S&T. Thank you, Jack Kane.
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K450BB 75 302 100 0.8816 2.8349 Animal_Motor_Works
|
||||
0.03 78.903
|
||||
0.045 227.9
|
||||
0.064 449.955
|
||||
0.069 508.417
|
||||
0.094 555.187
|
||||
0.151 563.956
|
||||
0.362 625.442
|
||||
0.562 651.85
|
||||
0.825 660.62
|
||||
1.134 652.254
|
||||
1.453 626.147
|
||||
1.793 594.296
|
||||
2.113 538.958
|
||||
2.458 469.106
|
||||
2.798 384.538
|
||||
3.165 276.686
|
||||
3.201 279.609
|
||||
3.325 232.94
|
||||
3.51 171.757
|
||||
3.732 107.65
|
||||
3.861 58.018
|
||||
3.959 40.55
|
||||
4.036 20.149
|
||||
4.11 0
|
||||
36
datafiles/thrustcurves/AMW_K470.eng
Normal file
36
datafiles/thrustcurves/AMW_K470.eng
Normal file
@ -0,0 +1,36 @@
|
||||
;
|
||||
;AMW K470ST RASP.ENG file made from Tripoli published data
|
||||
;File produced May 15, 2004
|
||||
;This file my be used or given away. All I ask is that this header
|
||||
;is maintained to give credit to the people who produced the data.
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K470ST 75 302 100 0.826 2.779 Animal_Motor_Works
|
||||
0.028 699.309
|
||||
0.039 799.337
|
||||
0.09 765.845
|
||||
0.157 770.311
|
||||
0.258 785.941
|
||||
0.41 804
|
||||
0.572 794.425
|
||||
0.707 794.425
|
||||
0.886 792.192
|
||||
0.998 783.261
|
||||
1.15 752.002
|
||||
1.318 709.579
|
||||
1.447 655.992
|
||||
1.593 595.707
|
||||
1.728 522.025
|
||||
1.885 444.101
|
||||
2.092 354.923
|
||||
2.356 270.167
|
||||
2.664 187.554
|
||||
2.945 131.734
|
||||
3.27 78.058
|
||||
3.433 55.686
|
||||
3.478 48.987
|
||||
3.556 28.909
|
||||
3.7 0
|
||||
38
datafiles/thrustcurves/AMW_K475.eng
Normal file
38
datafiles/thrustcurves/AMW_K475.eng
Normal file
@ -0,0 +1,38 @@
|
||||
;
|
||||
;Animal Motor Works K475 RASP.ENG file made from NAR data
|
||||
;File produced Feb 22, 2003
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K475WW 54 403 100 0.7286 1.4925 Animal_Motor_Works
|
||||
0.022 127.831
|
||||
0.041 386.016
|
||||
0.063 548.326
|
||||
0.096 521.308
|
||||
0.134 499.129
|
||||
0.18 486.83
|
||||
0.285 486.83
|
||||
0.478 501.649
|
||||
0.731 523.727
|
||||
1.096 553.266
|
||||
1.433 577.962
|
||||
1.601 588.29
|
||||
1.756 582.704
|
||||
1.895 580.284
|
||||
1.958 575.344
|
||||
2.063 550.746
|
||||
2.209 518.788
|
||||
2.344 477.051
|
||||
2.495 417.974
|
||||
2.561 354.058
|
||||
2.582 334.399
|
||||
2.599 331.98
|
||||
2.62 297.501
|
||||
2.67 226.226
|
||||
2.707 157.37
|
||||
2.74 98.353
|
||||
2.799 49.176
|
||||
2.853 17.208
|
||||
2.94 0
|
||||
43
datafiles/thrustcurves/AMW_K530.eng
Normal file
43
datafiles/thrustcurves/AMW_K530.eng
Normal file
@ -0,0 +1,43 @@
|
||||
;
|
||||
;Animal Motor Works 54-1400
|
||||
;AMW K530GG RASP.ENG file made from NAR data
|
||||
;File produced Feb 25, 2003
|
||||
;This file my be used or given away. All I ask is that this header
|
||||
;is maintained to give credit to NAR S&T. Thank you, Jack Kane
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K530GG 54 403 1000 0.7967 1.616 Animal_Motor_Works
|
||||
0.013 129.764
|
||||
0.054 171.852
|
||||
0.096 284.122
|
||||
0.138 392.892
|
||||
0.171 455.975
|
||||
0.217 501.662
|
||||
0.238 498.063
|
||||
0.326 508.66
|
||||
0.542 564.745
|
||||
0.755 613.831
|
||||
1.01 645.423
|
||||
1.17 657.23
|
||||
1.273 648.922
|
||||
1.51 638.425
|
||||
1.656 634.925
|
||||
1.702 606.833
|
||||
1.803 606.833
|
||||
1.857 585.839
|
||||
1.936 589.338
|
||||
1.974 575.242
|
||||
2.015 589.338
|
||||
2.04 564.745
|
||||
2.132 536.652
|
||||
2.207 540.251
|
||||
2.291 522.656
|
||||
2.357 487.566
|
||||
2.42 375.297
|
||||
2.478 242.033
|
||||
2.529 140.361
|
||||
2.583 66.651
|
||||
2.66 0
|
||||
33
datafiles/thrustcurves/AMW_K555.eng
Normal file
33
datafiles/thrustcurves/AMW_K555.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;Animal Motor Works 54-1750 K555 skidmark
|
||||
;File provide by Joel Rogers of AMW
|
||||
K555SK 54 492 0 0.8707 1.7343 AMW
|
||||
0.063 507.328
|
||||
0.144 535.181
|
||||
0.226 559.826
|
||||
0.308 585.793
|
||||
0.389 607.239
|
||||
0.471 629.034
|
||||
0.553 664.586
|
||||
0.634 683.688
|
||||
0.716 697.625
|
||||
0.798 719.618
|
||||
0.879 756.521
|
||||
0.961 777.700
|
||||
1.043 789.004
|
||||
1.124 797.934
|
||||
1.206 801.689
|
||||
1.288 804.331
|
||||
1.369 799.414
|
||||
1.451 768.014
|
||||
1.533 704.469
|
||||
1.614 641.709
|
||||
1.696 568.727
|
||||
1.778 481.013
|
||||
1.859 401.614
|
||||
1.941 333.897
|
||||
2.023 277.226
|
||||
2.104 205.009
|
||||
2.186 129.425
|
||||
2.268 73.717
|
||||
2.349 22.380
|
||||
2.368 0.000
|
||||
37
datafiles/thrustcurves/AMW_K560.eng
Normal file
37
datafiles/thrustcurves/AMW_K560.eng
Normal file
@ -0,0 +1,37 @@
|
||||
;
|
||||
;AMW K560 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K560RR 54 430 100 0.75 1.5866 Animal_Motor_Works
|
||||
0.023 229.13
|
||||
0.046 415.135
|
||||
0.059 485.264
|
||||
0.078 512.268
|
||||
0.106 525.67
|
||||
0.154 523.05
|
||||
0.211 528.39
|
||||
0.261 536.451
|
||||
0.369 560.734
|
||||
0.511 587.738
|
||||
0.657 603.86
|
||||
0.77 612.022
|
||||
1.096 625.75
|
||||
1.358 620.083
|
||||
1.627 612.022
|
||||
1.839 603.86
|
||||
2.057 590.459
|
||||
2.218 598.52
|
||||
2.335 609.301
|
||||
2.385 601.24
|
||||
2.407 585.018
|
||||
2.426 533.831
|
||||
2.467 385.511
|
||||
2.507 283.037
|
||||
2.542 164.441
|
||||
2.576 67.399
|
||||
2.595 29.653
|
||||
2.62 0
|
||||
28
datafiles/thrustcurves/AMW_K570.eng
Normal file
28
datafiles/thrustcurves/AMW_K570.eng
Normal file
@ -0,0 +1,28 @@
|
||||
;
|
||||
;Animal Motor Works K570 White Wolf
|
||||
K570WW 54 492 0 0.9146 1.8151 AMW
|
||||
0.020 364.42
|
||||
0.030 664.79
|
||||
0.051 751.47
|
||||
0.071 745.81
|
||||
0.096 705.25
|
||||
0.137 674.93
|
||||
0.284 661.38
|
||||
0.528 651.24
|
||||
0.913 644.51
|
||||
1.192 651.24
|
||||
1.430 651.24
|
||||
1.649 651.24
|
||||
1.872 644.51
|
||||
2.176 624.23
|
||||
2.318 600.64
|
||||
2.394 597.33
|
||||
2.455 546.63
|
||||
2.501 485.89
|
||||
2.562 421.84
|
||||
2.597 340.83
|
||||
2.638 266.54
|
||||
2.734 175.48
|
||||
2.836 97.86
|
||||
2.927 47.24
|
||||
3.040 0.00
|
||||
40
datafiles/thrustcurves/AMW_K600.eng
Normal file
40
datafiles/thrustcurves/AMW_K600.eng
Normal file
@ -0,0 +1,40 @@
|
||||
;
|
||||
; Animal Motor Works K600 RASP.ENG file made from NAR data
|
||||
; File produced August 22, 2002
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
K600 75 368 P 1.2233 2.9129 AMW
|
||||
0.010 412.229
|
||||
0.029 522.21
|
||||
0.059 547.215
|
||||
0.083 524.8
|
||||
0.122 497.305
|
||||
0.181 484.852
|
||||
0.333 495.113
|
||||
0.690 560.464
|
||||
1.195 643.548
|
||||
1.400 673.833
|
||||
1.420 708.799
|
||||
1.508 701.427
|
||||
1.591 721.551
|
||||
1.782 731.712
|
||||
2.017 752.035
|
||||
2.174 756.816
|
||||
2.257 765.2
|
||||
2.502 766.44
|
||||
2.727 752.931
|
||||
2.918 738.187
|
||||
3.143 705.91
|
||||
3.408 643.847
|
||||
3.603 569.131
|
||||
3.692 526.793
|
||||
3.745 439.426
|
||||
3.799 289.596
|
||||
3.883 112.272
|
||||
3.922 64.862
|
||||
3.971 37.437
|
||||
3.995 22.474
|
||||
4.070 0
|
||||
34
datafiles/thrustcurves/AMW_K600_1.eng
Normal file
34
datafiles/thrustcurves/AMW_K600_1.eng
Normal file
@ -0,0 +1,34 @@
|
||||
;
|
||||
;Animal Motor Works K600 White Wolf
|
||||
K600WW 75 368 0 1.2233 2.9129 AMW
|
||||
0.010 412.229
|
||||
0.029 522.21
|
||||
0.059 547.215
|
||||
0.083 524.8
|
||||
0.122 497.305
|
||||
0.181 484.852
|
||||
0.333 495.113
|
||||
0.690 560.464
|
||||
1.195 643.548
|
||||
1.400 673.833
|
||||
1.420 708.799
|
||||
1.508 701.427
|
||||
1.591 721.551
|
||||
1.782 731.712
|
||||
2.017 752.035
|
||||
2.174 756.816
|
||||
2.257 765.2
|
||||
2.502 766.44
|
||||
2.727 752.931
|
||||
2.918 738.187
|
||||
3.143 705.91
|
||||
3.408 643.847
|
||||
3.603 569.131
|
||||
3.692 526.793
|
||||
3.745 439.426
|
||||
3.799 289.596
|
||||
3.883 112.272
|
||||
3.922 64.862
|
||||
3.971 37.437
|
||||
3.995 22.474
|
||||
4.070 0
|
||||
31
datafiles/thrustcurves/AMW_K605.eng
Normal file
31
datafiles/thrustcurves/AMW_K605.eng
Normal file
@ -0,0 +1,31 @@
|
||||
;
|
||||
;AMW K605 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K605RR 75 368 100 1.231 2.7688 Animal_Motor_Works
|
||||
0.03 165.845
|
||||
0.053 309.12
|
||||
0.077 361.916
|
||||
0.142 392.042
|
||||
0.527 501.412
|
||||
0.988 606.905
|
||||
1.515 682.37
|
||||
2.101 730.593
|
||||
2.355 737.58
|
||||
2.692 731.289
|
||||
3 712.497
|
||||
3.361 671.036
|
||||
3.503 663.479
|
||||
3.586 659.701
|
||||
3.645 633.353
|
||||
3.692 573
|
||||
3.734 444.838
|
||||
3.775 297.785
|
||||
3.828 162.066
|
||||
3.864 98.015
|
||||
3.905 41.471
|
||||
3.95 0
|
||||
38
datafiles/thrustcurves/AMW_K650.eng
Normal file
38
datafiles/thrustcurves/AMW_K650.eng
Normal file
@ -0,0 +1,38 @@
|
||||
; Animal Motor Works 54-1750
|
||||
; AMW K650RR RASP.ENG file made from NAR published data
|
||||
; File produced April 19, 2004
|
||||
; This file my be used or given away. All I ask is that this header
|
||||
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
K650RR 54 492 0 0.931 1.8087 AMW
|
||||
0.022 308.257
|
||||
0.045 566.480
|
||||
0.058 620.440
|
||||
0.081 639.668
|
||||
0.135 639.668
|
||||
0.229 643.494
|
||||
0.351 662.823
|
||||
0.594 701.380
|
||||
0.810 724.434
|
||||
0.999 743.763
|
||||
1.151 751.220
|
||||
1.381 747.588
|
||||
1.610 736.001
|
||||
1.835 709.031
|
||||
2.073 685.876
|
||||
2.244 674.400
|
||||
2.334 682.051
|
||||
2.429 685.876
|
||||
2.469 666.648
|
||||
2.528 597.285
|
||||
2.573 481.714
|
||||
2.609 358.391
|
||||
2.631 250.471
|
||||
2.681 146.477
|
||||
2.721 65.507
|
||||
2.748 23.124
|
||||
2.770 0.000
|
||||
34
datafiles/thrustcurves/AMW_K670.eng
Normal file
34
datafiles/thrustcurves/AMW_K670.eng
Normal file
@ -0,0 +1,34 @@
|
||||
;
|
||||
; AMW K670 RASP.ENG file made from NAR published data
|
||||
; File produced SEPT 4, 2002
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
K670 54 492 P- 1.0140 1.9145 AMW
|
||||
0.016 294.05
|
||||
0.035 398.577
|
||||
0.086 506.292
|
||||
0.153 496.428
|
||||
0.264 506.093
|
||||
0.461 558.108
|
||||
0.722 629.553
|
||||
0.983 688.044
|
||||
1.116 714.051
|
||||
1.193 785.795
|
||||
1.409 788.784
|
||||
1.737 804.56
|
||||
2.074 781.41
|
||||
2.195 764.87
|
||||
2.226 781.211
|
||||
2.277 764.77
|
||||
2.398 751.517
|
||||
2.440 744.941
|
||||
2.468 718.834
|
||||
2.484 666.521
|
||||
2.525 418.107
|
||||
2.551 218.818
|
||||
2.573 120.768
|
||||
2.595 52.143
|
||||
2.620 0
|
||||
28
datafiles/thrustcurves/AMW_K670_1.eng
Normal file
28
datafiles/thrustcurves/AMW_K670_1.eng
Normal file
@ -0,0 +1,28 @@
|
||||
;
|
||||
;Animal Motor Works K670 Green Gorilla
|
||||
K670GG 54 492 0 1.0140 1.9145 AMW
|
||||
0.016 294.05
|
||||
0.035 398.577
|
||||
0.086 506.292
|
||||
0.153 496.428
|
||||
0.264 506.093
|
||||
0.461 558.108
|
||||
0.722 629.553
|
||||
0.983 688.044
|
||||
1.116 714.051
|
||||
1.193 785.795
|
||||
1.409 788.784
|
||||
1.737 804.56
|
||||
2.074 781.41
|
||||
2.195 764.87
|
||||
2.226 781.211
|
||||
2.277 764.77
|
||||
2.398 751.517
|
||||
2.440 744.941
|
||||
2.468 718.834
|
||||
2.484 666.521
|
||||
2.525 418.107
|
||||
2.551 218.818
|
||||
2.573 120.768
|
||||
2.595 52.143
|
||||
2.620 0
|
||||
36
datafiles/thrustcurves/AMW_K700.eng
Normal file
36
datafiles/thrustcurves/AMW_K700.eng
Normal file
@ -0,0 +1,36 @@
|
||||
;
|
||||
;AMW K700 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
K700BB 54 430 100 0.754 1.4831 Animal_Motor_Works
|
||||
0.014 359.559
|
||||
0.022 625.425
|
||||
0.03 737.756
|
||||
0.047 771.505
|
||||
0.082 786.516
|
||||
0.106 771.505
|
||||
0.144 775.233
|
||||
0.272 786.516
|
||||
0.477 812.71
|
||||
0.693 842.632
|
||||
0.97 847.06
|
||||
1.283 838.904
|
||||
1.516 816.438
|
||||
1.706 801.427
|
||||
1.779 793.972
|
||||
1.811 775.233
|
||||
1.841 726.573
|
||||
1.873 625.425
|
||||
1.909 509.367
|
||||
1.95 393.208
|
||||
1.982 337.093
|
||||
2.035 292.16
|
||||
2.073 228.489
|
||||
2.111 153.535
|
||||
2.155 86.137
|
||||
2.193 37.446
|
||||
2.24 0
|
||||
35
datafiles/thrustcurves/AMW_K800.eng
Normal file
35
datafiles/thrustcurves/AMW_K800.eng
Normal file
@ -0,0 +1,35 @@
|
||||
; This file my be used or given away. All I ask is that this header
|
||||
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
K800BB 54 492 0 0.9140 1.7866 AMW
|
||||
0.017 516.316
|
||||
0.035 745.845
|
||||
0.046 817.592
|
||||
0.090 860.560
|
||||
0.191 889.338
|
||||
0.270 908.424
|
||||
0.438 918.017
|
||||
0.689 945.892
|
||||
0.996 955.090
|
||||
1.325 922.713
|
||||
1.557 894.035
|
||||
1.726 874.949
|
||||
1.849 884.542
|
||||
1.920 894.035
|
||||
1.954 894.035
|
||||
1.984 855.863
|
||||
2.011 741.048
|
||||
2.049 592.859
|
||||
2.079 492.433
|
||||
2.113 430.280
|
||||
2.154 377.719
|
||||
2.196 329.854
|
||||
2.237 243.818
|
||||
2.275 152.986
|
||||
2.309 71.716
|
||||
2.339 33.465
|
||||
2.380 0.000
|
||||
39
datafiles/thrustcurves/AMW_K950.eng
Normal file
39
datafiles/thrustcurves/AMW_K950.eng
Normal file
@ -0,0 +1,39 @@
|
||||
;
|
||||
; AMW K950 RASP.ENG file made from NAR published data
|
||||
; File produced SEPT 4, 2002
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
K950 54 492 P .8874 1.7949 AMW
|
||||
0.011 771.836
|
||||
0.025 1204.520
|
||||
0.039 1083.244
|
||||
0.053 1158.054
|
||||
0.067 1036.364
|
||||
0.085 1110.176
|
||||
0.099 1022.399
|
||||
0.135 982.102
|
||||
0.220 968.835
|
||||
0.404 1010.430
|
||||
0.566 1044.343
|
||||
0.701 1079.254
|
||||
0.867 1106.186
|
||||
0.995 1134.115
|
||||
1.211 1114.166
|
||||
1.313 1101.199
|
||||
1.430 1067.285
|
||||
1.529 1020.404
|
||||
1.579 993.772
|
||||
1.642 892.430
|
||||
1.674 818.119
|
||||
1.717 757.273
|
||||
1.738 621.918
|
||||
1.766 466.313
|
||||
1.791 351.306
|
||||
1.823 249.864
|
||||
1.865 175.553
|
||||
1.908 87.696
|
||||
1.943 33.654
|
||||
1.970 0.000
|
||||
33
datafiles/thrustcurves/AMW_K950_1.eng
Normal file
33
datafiles/thrustcurves/AMW_K950_1.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;
|
||||
;Animal Motor Works K950 Super Tiger
|
||||
K950ST 54 492 0 .8874 1.7949 AMW
|
||||
0.011 771.836
|
||||
0.025 1204.520
|
||||
0.039 1083.244
|
||||
0.053 1158.054
|
||||
0.067 1036.364
|
||||
0.085 1110.176
|
||||
0.099 1022.399
|
||||
0.135 982.102
|
||||
0.220 968.835
|
||||
0.404 1010.430
|
||||
0.566 1044.343
|
||||
0.701 1079.254
|
||||
0.867 1106.186
|
||||
0.995 1134.115
|
||||
1.211 1114.166
|
||||
1.313 1101.199
|
||||
1.430 1067.285
|
||||
1.529 1020.404
|
||||
1.579 993.772
|
||||
1.642 892.430
|
||||
1.674 818.119
|
||||
1.717 757.273
|
||||
1.738 621.918
|
||||
1.766 466.313
|
||||
1.791 351.306
|
||||
1.823 249.864
|
||||
1.865 175.553
|
||||
1.908 87.696
|
||||
1.943 33.654
|
||||
1.970 0.000
|
||||
35
datafiles/thrustcurves/AMW_K975.eng
Normal file
35
datafiles/thrustcurves/AMW_K975.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;Animal Motor Works K975 White Wolf
|
||||
K975WW 54 728 0 1.357 2.5985 AMW
|
||||
0.017 526.644
|
||||
0.029 901.850
|
||||
0.038 1098.918
|
||||
0.046 1151.722
|
||||
0.076 1112.867
|
||||
0.130 1060.063
|
||||
0.219 1053.089
|
||||
0.336 1053.089
|
||||
0.479 1059.066
|
||||
0.609 1091.944
|
||||
0.866 1136.778
|
||||
1.046 1176.630
|
||||
1.164 1175.634
|
||||
1.202 1228.437
|
||||
1.239 1208.511
|
||||
1.315 1215.486
|
||||
1.353 1267.293
|
||||
1.387 1228.437
|
||||
1.487 1241.389
|
||||
1.538 1260.319
|
||||
1.634 1290.900
|
||||
1.723 1281.241
|
||||
1.794 1266.297
|
||||
1.836 1207.515
|
||||
1.933 1049.103
|
||||
1.992 851.437
|
||||
2.080 666.923
|
||||
2.118 640.521
|
||||
2.193 462.582
|
||||
2.269 212.311
|
||||
2.378 119.854
|
||||
2.510 0.000
|
||||
39
datafiles/thrustcurves/AMW_L1060.eng
Normal file
39
datafiles/thrustcurves/AMW_L1060.eng
Normal file
@ -0,0 +1,39 @@
|
||||
;
|
||||
; AMW L1060 RASP.ENG file made from NAR published data
|
||||
; File produced August 22, 2002
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
L1060 75 497 P- 1.9188 3.9388 AMW
|
||||
0.020 258.773
|
||||
0.024 368.235
|
||||
0.032 328.386
|
||||
0.076 427.96
|
||||
0.100 567.284
|
||||
0.116 751.352
|
||||
0.128 791.202
|
||||
0.169 816.071
|
||||
0.225 816.071
|
||||
0.309 875.795
|
||||
0.518 985.257
|
||||
0.763 1079.639
|
||||
1.024 1174.519
|
||||
1.308 1229.45
|
||||
1.606 1288.375
|
||||
1.782 1298.25
|
||||
1.983 1293.369
|
||||
2.256 1239.437
|
||||
2.525 1184.506
|
||||
2.822 1129.576
|
||||
3.038 1069.651
|
||||
3.111 1044.683
|
||||
3.135 995.145
|
||||
3.183 835.946
|
||||
3.239 552.303
|
||||
3.299 268.661
|
||||
3.327 164.193
|
||||
3.339 84.593
|
||||
3.360 44.783
|
||||
3.400 0
|
||||
33
datafiles/thrustcurves/AMW_L1060_1.eng
Normal file
33
datafiles/thrustcurves/AMW_L1060_1.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;
|
||||
;Animal Motor Works L1060 Green Gorilla
|
||||
L1060GG 75 497 0 1.9188 3.9388 AMW
|
||||
0.020 258.773
|
||||
0.024 368.235
|
||||
0.032 328.386
|
||||
0.076 427.96
|
||||
0.100 567.284
|
||||
0.116 751.352
|
||||
0.128 791.202
|
||||
0.169 816.071
|
||||
0.225 816.071
|
||||
0.309 875.795
|
||||
0.518 985.257
|
||||
0.763 1079.639
|
||||
1.024 1174.519
|
||||
1.308 1229.45
|
||||
1.606 1288.375
|
||||
1.782 1298.25
|
||||
1.983 1293.369
|
||||
2.256 1239.437
|
||||
2.525 1184.506
|
||||
2.822 1129.576
|
||||
3.038 1069.651
|
||||
3.111 1044.683
|
||||
3.135 995.145
|
||||
3.183 835.946
|
||||
3.239 552.303
|
||||
3.299 268.661
|
||||
3.327 164.193
|
||||
3.339 84.593
|
||||
3.360 44.783
|
||||
3.400 0
|
||||
35
datafiles/thrustcurves/AMW_L1080.eng
Normal file
35
datafiles/thrustcurves/AMW_L1080.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;AMW L1080 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
L1080BB 75 497 100 1.717 3.5922 Animal_Motor_Works
|
||||
0.024 406.295
|
||||
0.043 812.489
|
||||
0.052 895.202
|
||||
0.088 929.641
|
||||
0.314 991.55
|
||||
0.626 1087.69
|
||||
0.988 1163.44
|
||||
1.346 1218.99
|
||||
1.638 1246.25
|
||||
1.864 1257.91
|
||||
2.247 1254.84
|
||||
2.6 1218.99
|
||||
2.766 1211.92
|
||||
2.851 1197.78
|
||||
2.942 1204.85
|
||||
3.002 1226.06
|
||||
3.033 1204.85
|
||||
3.089 1040.23
|
||||
3.124 874.499
|
||||
3.15 660.999
|
||||
3.191 461.336
|
||||
3.232 275.408
|
||||
3.268 144.622
|
||||
3.303 75.744
|
||||
3.339 41.316
|
||||
3.39 0
|
||||
33
datafiles/thrustcurves/AMW_L1100.eng
Normal file
33
datafiles/thrustcurves/AMW_L1100.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;
|
||||
;AMW L1100 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
L1100RR 75 728 100 1.346 2.5881 Animal_Motor_Works
|
||||
0.013 681.489
|
||||
0.029 1116.88
|
||||
0.041 1196.3
|
||||
0.079 1210.38
|
||||
0.147 1203.34
|
||||
0.257 1218.42
|
||||
0.366 1225.45
|
||||
0.567 1254.61
|
||||
0.824 1282.76
|
||||
1.059 1311.91
|
||||
1.267 1340.23
|
||||
1.459 1311.91
|
||||
1.622 1297.84
|
||||
1.713 1290.8
|
||||
1.785 1268.68
|
||||
1.83 1218.42
|
||||
1.886 1080.69
|
||||
1.969 819.214
|
||||
2.048 558.24
|
||||
2.108 376.985
|
||||
2.156 246.498
|
||||
2.205 144.963
|
||||
2.269 72.501
|
||||
2.35 0
|
||||
26
datafiles/thrustcurves/AMW_L1111.eng
Normal file
26
datafiles/thrustcurves/AMW_L1111.eng
Normal file
@ -0,0 +1,26 @@
|
||||
;
|
||||
;L1111ST entered by Tim Van Milligan
|
||||
;For RockSim - http://www.rocksim.com
|
||||
;Based on TRA Certification paperwork from 06-01-2002
|
||||
;Initial Mass from Jim Robinson at AMW
|
||||
;Not approved by TRA or AMW.
|
||||
L1111ST 75 497 100 1.642 3.517 Animal_Motor_Works
|
||||
0.015 1023.97
|
||||
0.1 924.878
|
||||
0.147 902.857
|
||||
0.502 1034.98
|
||||
0.75 1156.1
|
||||
1.005 1266.2
|
||||
1.229 1354.29
|
||||
1.492 1398.33
|
||||
1.739 1398.33
|
||||
2.009 1354.29
|
||||
2.272 1244.18
|
||||
2.504 1123.07
|
||||
2.728 968.92
|
||||
2.782 902.857
|
||||
2.836 770.732
|
||||
2.98 363.345
|
||||
3.053 99.094
|
||||
3.083 22.021
|
||||
3.14 0
|
||||
35
datafiles/thrustcurves/AMW_L1300.eng
Normal file
35
datafiles/thrustcurves/AMW_L1300.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;AMW L1300 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
L1300BB 75 728 100 1.314 2.5454 Animal_Motor_Works
|
||||
0.014 710.467
|
||||
0.025 1247.64
|
||||
0.039 1384.13
|
||||
0.053 1447.83
|
||||
0.074 1420.53
|
||||
0.12 1447.83
|
||||
0.276 1474.12
|
||||
0.475 1519.61
|
||||
0.712 1555
|
||||
0.942 1586.74
|
||||
1.147 1562.08
|
||||
1.36 1534.78
|
||||
1.484 1551.97
|
||||
1.537 1551.97
|
||||
1.569 1497.37
|
||||
1.59 1406.38
|
||||
1.604 1451.87
|
||||
1.615 1333.58
|
||||
1.64 1168.78
|
||||
1.689 986.687
|
||||
1.753 767.749
|
||||
1.824 512.503
|
||||
1.891 275.512
|
||||
1.933 147.816
|
||||
1.987 74.737
|
||||
2.06 0
|
||||
35
datafiles/thrustcurves/AMW_L1400.eng
Normal file
35
datafiles/thrustcurves/AMW_L1400.eng
Normal file
@ -0,0 +1,35 @@
|
||||
; @File: SK-75-6000.txt, @Pts-I: 3609, @Pts-O: 31, @Sm: 6, @CO: 5%
|
||||
; @TI: 4740.56, @TIa: 4732.91, @TIe: 0.0%, @ThMax: 1908.398, @ThAvg: 1382.678, @Tb: 3.423
|
||||
; Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar
|
||||
L1400SK 75 785 P 2.8267 5.1985 AMW
|
||||
0.0 68.1234
|
||||
0.0040 193.7893
|
||||
0.016 690.259
|
||||
0.021 814.579
|
||||
0.027 900.741
|
||||
0.045 997.475
|
||||
0.076 1251.156
|
||||
0.092 1354.553
|
||||
0.107 1405.971
|
||||
0.132 1440.082
|
||||
0.169 1453.774
|
||||
0.368 1397.446
|
||||
0.525 1411.875
|
||||
0.705 1488.288
|
||||
1.082 1734.489
|
||||
1.414 1906.629
|
||||
1.556 1875.238
|
||||
1.766 1882.261
|
||||
1.899 1803.008
|
||||
2.142 1745.497
|
||||
2.34 1659.082
|
||||
2.504 1522.458
|
||||
2.58 1402.287
|
||||
2.819 844.839
|
||||
2.847 841.674
|
||||
2.893 730.795
|
||||
3.068 406.536
|
||||
3.176 265.8
|
||||
3.425 94.9644
|
||||
3.608 0.874524
|
||||
3.609 0
|
||||
34
datafiles/thrustcurves/AMW_L666.eng
Normal file
34
datafiles/thrustcurves/AMW_L666.eng
Normal file
@ -0,0 +1,34 @@
|
||||
;Animal Motor Works 75-3500
|
||||
L666SK 75 497 0 1.8877 3.5344 AMW
|
||||
0.096 105.880
|
||||
0.175 509.783
|
||||
0.312 549.481
|
||||
0.449 577.319
|
||||
0.586 602.900
|
||||
0.722 615.605
|
||||
0.859 632.540
|
||||
0.996 652.072
|
||||
1.133 671.418
|
||||
1.270 685.671
|
||||
1.407 701.286
|
||||
1.543 718.069
|
||||
1.680 734.116
|
||||
1.817 753.292
|
||||
1.954 771.589
|
||||
2.091 790.453
|
||||
2.228 819.222
|
||||
2.364 846.663
|
||||
2.501 874.629
|
||||
2.638 890.083
|
||||
2.775 898.271
|
||||
2.912 899.312
|
||||
3.049 881.683
|
||||
3.185 845.157
|
||||
3.322 768.451
|
||||
3.459 672.771
|
||||
3.596 525.466
|
||||
3.733 304.694
|
||||
3.870 86.663
|
||||
3.968 0.000
|
||||
;
|
||||
;
|
||||
29
datafiles/thrustcurves/AMW_L700.eng
Normal file
29
datafiles/thrustcurves/AMW_L700.eng
Normal file
@ -0,0 +1,29 @@
|
||||
;
|
||||
;
|
||||
L700BB 75.0 368.00 100 1.19310 2.73200 AMW
|
||||
0.02 221.87
|
||||
0.03 399.33
|
||||
0.05 467.56
|
||||
0.08 494.89
|
||||
0.13 498.41
|
||||
0.24 535.99
|
||||
0.48 614.67
|
||||
0.77 683.20
|
||||
1.23 755.25
|
||||
1.62 789.72
|
||||
1.92 810.42
|
||||
2.26 821.14
|
||||
2.58 817.85
|
||||
2.91 801.07
|
||||
3.14 773.94
|
||||
3.25 750.13
|
||||
3.32 743.39
|
||||
3.37 729.83
|
||||
3.42 688.83
|
||||
3.46 593.37
|
||||
3.50 484.14
|
||||
3.53 368.18
|
||||
3.57 248.80
|
||||
3.62 149.82
|
||||
3.66 61.13
|
||||
3.72 0.00
|
||||
40
datafiles/thrustcurves/AMW_L777.eng
Normal file
40
datafiles/thrustcurves/AMW_L777.eng
Normal file
@ -0,0 +1,40 @@
|
||||
;
|
||||
; AMW L777 RASP.ENG file made from NAR published data
|
||||
; File produced SEPT 4, 2002
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
L777 75 497 P 1.7623 3.6987 AMW
|
||||
0.025 140.882
|
||||
0.064 209.474
|
||||
0.108 360.055
|
||||
0.204 652.185
|
||||
0.360 641.518
|
||||
0.373 693.745
|
||||
0.418 683.28
|
||||
0.528 730.073
|
||||
0.670 761.268
|
||||
0.761 781.998
|
||||
0.787 802.828
|
||||
0.871 802.728
|
||||
1.065 854.754
|
||||
1.338 911.811
|
||||
1.668 963.636
|
||||
1.914 989.498
|
||||
2.115 1000.16
|
||||
2.368 962.831
|
||||
2.647 926
|
||||
2.985 878.603
|
||||
3.303 805.143
|
||||
3.472 752.815
|
||||
3.550 705.72
|
||||
3.602 648.26
|
||||
3.647 611.631
|
||||
3.693 512.409
|
||||
3.779 334.897
|
||||
3.857 178.216
|
||||
3.935 89.379
|
||||
3.981 26.687
|
||||
4.050 0
|
||||
34
datafiles/thrustcurves/AMW_L777_1.eng
Normal file
34
datafiles/thrustcurves/AMW_L777_1.eng
Normal file
@ -0,0 +1,34 @@
|
||||
;
|
||||
;Animal Motor Works L777 White Wolf
|
||||
L777WW 75 497 0 1.7623 3.6987 AMW
|
||||
0.025 140.882
|
||||
0.064 209.474
|
||||
0.108 360.055
|
||||
0.204 652.185
|
||||
0.360 641.518
|
||||
0.373 693.745
|
||||
0.418 683.28
|
||||
0.528 730.073
|
||||
0.670 761.268
|
||||
0.761 781.998
|
||||
0.787 802.828
|
||||
0.871 802.728
|
||||
1.065 854.754
|
||||
1.338 911.811
|
||||
1.668 963.636
|
||||
1.914 989.498
|
||||
2.115 1000.16
|
||||
2.368 962.831
|
||||
2.647 926
|
||||
2.985 878.603
|
||||
3.303 805.143
|
||||
3.472 752.815
|
||||
3.550 705.72
|
||||
3.602 648.26
|
||||
3.647 611.631
|
||||
3.693 512.409
|
||||
3.779 334.897
|
||||
3.857 178.216
|
||||
3.935 89.379
|
||||
3.981 26.687
|
||||
4.050 0
|
||||
37
datafiles/thrustcurves/AMW_L900.eng
Normal file
37
datafiles/thrustcurves/AMW_L900.eng
Normal file
@ -0,0 +1,37 @@
|
||||
;
|
||||
;AMW L900 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
L900RR 75 497 100 1.771 3.5888 Animal_Motor_Works
|
||||
0.029 464.292
|
||||
0.053 630.937
|
||||
0.059 684.506
|
||||
0.096 702.328
|
||||
0.133 696.387
|
||||
0.201 714.311
|
||||
0.486 803.524
|
||||
0.777 910.661
|
||||
1.099 988.093
|
||||
1.26 1041.16
|
||||
1.284 1071.37
|
||||
1.378 1053.24
|
||||
1.607 1101.57
|
||||
1.917 1142.86
|
||||
2.208 1173.56
|
||||
2.413 1160.98
|
||||
2.624 1107.62
|
||||
2.866 976.211
|
||||
3.053 886.897
|
||||
3.208 839.27
|
||||
3.314 827.388
|
||||
3.382 809.465
|
||||
3.432 720.252
|
||||
3.495 547.564
|
||||
3.57 345.273
|
||||
3.627 214.273
|
||||
3.714 77.382
|
||||
3.79 0
|
||||
21
datafiles/thrustcurves/AMW_M1350.eng
Normal file
21
datafiles/thrustcurves/AMW_M1350.eng
Normal file
@ -0,0 +1,21 @@
|
||||
;
|
||||
;Animal Motor Works M1350 White Wolf
|
||||
M1350WW 75 781 0 2.92700 5.40300 AMW
|
||||
0.03 1197.771588
|
||||
0.04 1465.181058
|
||||
0.07 1660.167131
|
||||
0.09 1665.738162
|
||||
0.16 1587.743733
|
||||
0.45 1587.743733
|
||||
0.61 1576.601671
|
||||
1.86 1649.02507
|
||||
2.27 1643.454039
|
||||
2.64 1598.885794
|
||||
3.18 1504.178273
|
||||
3.29 1353.760446
|
||||
3.41 991.643454
|
||||
3.49 841.2256267
|
||||
3.62 646.2395543
|
||||
3.74 428.9693593
|
||||
3.90 373.2590529
|
||||
4.22 0
|
||||
37
datafiles/thrustcurves/AMW_M1480.eng
Normal file
37
datafiles/thrustcurves/AMW_M1480.eng
Normal file
@ -0,0 +1,37 @@
|
||||
;
|
||||
;AMW M1480 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
M1480RR 75 785 100 3 5.5248 Animal_Motor_Works
|
||||
0.022 713.002
|
||||
0.032 1254.68
|
||||
0.055 1473.37
|
||||
0.078 1569.11
|
||||
0.156 1569.11
|
||||
0.352 1559.03
|
||||
0.642 1597.33
|
||||
0.974 1644.69
|
||||
1.289 1702.13
|
||||
1.52 1739.42
|
||||
1.918 1796.87
|
||||
2.279 1814.83
|
||||
2.481 1796.87
|
||||
2.707 1739.42
|
||||
2.968 1644.69
|
||||
3.058 1616.47
|
||||
3.135 1520.73
|
||||
3.218 1378.64
|
||||
3.284 1217.39
|
||||
3.332 1065.22
|
||||
3.344 1140.8
|
||||
3.368 1016.85
|
||||
3.41 741.522
|
||||
3.5 522.935
|
||||
3.613 275.727
|
||||
3.691 171.12
|
||||
3.768 66.553
|
||||
3.85 0
|
||||
36
datafiles/thrustcurves/AMW_M1730.eng
Normal file
36
datafiles/thrustcurves/AMW_M1730.eng
Normal file
@ -0,0 +1,36 @@
|
||||
;
|
||||
;Animal Motor Works 98-11000
|
||||
M1730SK 98 870 0 4.9452 9.8718 AMW
|
||||
0.040 682.642
|
||||
0.064 1153.387
|
||||
0.221 1354.665
|
||||
0.269 1414.771
|
||||
0.381 1458.026
|
||||
0.541 1526.924
|
||||
0.701 1589.200
|
||||
0.861 1675.203
|
||||
1.021 1732.669
|
||||
1.181 1802.227
|
||||
1.341 1886.644
|
||||
1.500 1973.713
|
||||
1.660 2070.514
|
||||
1.820 2183.822
|
||||
1.980 2299.313
|
||||
2.140 2433.862
|
||||
2.300 2568.119
|
||||
2.460 2679.423
|
||||
2.620 2638.376
|
||||
2.780 2484.185
|
||||
2.940 2306.038
|
||||
3.099 2173.849
|
||||
3.259 2074.688
|
||||
3.419 1961.303
|
||||
3.579 1807.810
|
||||
3.739 1640.258
|
||||
3.899 1303.035
|
||||
4.059 940.600
|
||||
4.219 567.152
|
||||
4.379 309.143
|
||||
4.539 188.981
|
||||
4.637 0.000
|
||||
;
|
||||
18
datafiles/thrustcurves/AMW_M1850.eng
Normal file
18
datafiles/thrustcurves/AMW_M1850.eng
Normal file
@ -0,0 +1,18 @@
|
||||
;
|
||||
; Animal Motor Works M1850GG
|
||||
; estimated from TRA graph by John DeMar jsdemar@syr.edu
|
||||
; motor mass is a guess based on similar types
|
||||
M1850GG 75 781 0 3.3750 4.5000 AMW
|
||||
0.08 979.00
|
||||
0.13 1180.00
|
||||
0.28 1290.00
|
||||
0.33 1468.00
|
||||
0.73 1936.00
|
||||
1.33 2202.00
|
||||
1.73 2279.00
|
||||
2.58 2105.00
|
||||
2.83 2007.00
|
||||
2.88 1860.00
|
||||
3.08 538.00
|
||||
3.20 174.00
|
||||
3.30 0.00
|
||||
30
datafiles/thrustcurves/AMW_M1850_1.eng
Normal file
30
datafiles/thrustcurves/AMW_M1850_1.eng
Normal file
@ -0,0 +1,30 @@
|
||||
;
|
||||
;Animal Motor Works M1850 Green Gorilla
|
||||
M1850GG 75 781 0 3.37000 5.85100 AMW
|
||||
0.12 1201.01994
|
||||
0.25 1321.121934
|
||||
0.37 1579.11881
|
||||
0.50 1699.220804
|
||||
0.62 1846.01213
|
||||
0.75 1930.528348
|
||||
0.87 1997.251678
|
||||
1.00 2059.526786
|
||||
1.12 2126.250116
|
||||
1.25 2192.973446
|
||||
1.37 2224.111
|
||||
1.50 2246.35211
|
||||
1.62 2268.59322
|
||||
1.75 2277.489664
|
||||
1.87 2268.59322
|
||||
2.00 2246.35211
|
||||
2.12 2224.111
|
||||
2.25 2192.973446
|
||||
2.37 2166.284114
|
||||
2.50 2144.043004
|
||||
2.62 2099.560784
|
||||
2.75 2046.18212
|
||||
2.87 1912.73546
|
||||
3.00 831.817514
|
||||
3.12 311.37554
|
||||
3.25 84.516218
|
||||
3.3 0.000
|
||||
38
datafiles/thrustcurves/AMW_M1900.eng
Normal file
38
datafiles/thrustcurves/AMW_M1900.eng
Normal file
@ -0,0 +1,38 @@
|
||||
;
|
||||
;AMW M1900 RASP.ENG file made from NAR published data
|
||||
;File produced April 19, 2004
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
M1900BB 75 785 100 2.733 5.4225 Animal_Motor_Works
|
||||
0.018 1109.21
|
||||
0.044 1761.75
|
||||
0.061 1910.65
|
||||
0.085 1938.62
|
||||
0.159 1929.63
|
||||
0.29 1956.62
|
||||
0.409 2031.56
|
||||
0.438 1974.6
|
||||
0.569 2011.58
|
||||
0.815 2104.51
|
||||
1.073 2197.44
|
||||
1.401 2280.39
|
||||
1.688 2324.7
|
||||
1.905 2297.37
|
||||
2.073 2241.41
|
||||
2.254 2138.49
|
||||
2.397 2063.54
|
||||
2.479 2016.57
|
||||
2.54 2025.57
|
||||
2.581 2006.58
|
||||
2.63 1885.67
|
||||
2.716 1493.94
|
||||
2.805 1120.21
|
||||
2.887 840.605
|
||||
2.972 569.996
|
||||
3.046 299.488
|
||||
3.119 150.193
|
||||
3.168 56.829
|
||||
3.23 0
|
||||
33
datafiles/thrustcurves/AMW_M2500.eng
Normal file
33
datafiles/thrustcurves/AMW_M2500.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;
|
||||
;Animal Motor Works M2500 Green Gorilla
|
||||
M2500GG 75 1039 0 4.248 7.5515 AMW
|
||||
0.026 1288.791
|
||||
0.053 2021.398
|
||||
0.079 2140.011
|
||||
0.123 2105.125
|
||||
0.207 2117.086
|
||||
0.540 2309.458
|
||||
0.971 2560.637
|
||||
1.265 2727.094
|
||||
1.480 2836.736
|
||||
1.678 2920.462
|
||||
1.757 2980.267
|
||||
1.946 2995.51
|
||||
2.047 2959.335
|
||||
2.240 2889.563
|
||||
2.310 2854.677
|
||||
2.486 2820.788
|
||||
2.526 2880.593
|
||||
2.592 2773.941
|
||||
2.653 2821.785
|
||||
2.706 2752.012
|
||||
2.758 2752.012
|
||||
2.807 2763.973
|
||||
2.842 2504.82
|
||||
2.886 2115.092
|
||||
2.930 1630.674
|
||||
2.987 1051.565
|
||||
3.040 437.571
|
||||
3.057 284.072
|
||||
3.079 142.434
|
||||
3.110 0
|
||||
32
datafiles/thrustcurves/AMW_M3000.eng
Normal file
32
datafiles/thrustcurves/AMW_M3000.eng
Normal file
@ -0,0 +1,32 @@
|
||||
;
|
||||
; Animal Motor Works M3000ST
|
||||
; estimated from TRA graph by Rob Bazinet rbazinet66@hotmail.com
|
||||
; motor mass is a guess based on similar types
|
||||
M3000ST 75 1038 0 3.8190 6.72 AMW
|
||||
0.032 2494.225
|
||||
0.113 2621.05
|
||||
0.242 2705.6
|
||||
0.355 2811.288
|
||||
0.435 2895.838
|
||||
0.5 2959.25
|
||||
0.645 3128.35
|
||||
0.75 3297.45
|
||||
0.871 3382
|
||||
0.968 3551.1
|
||||
1.032 3656.788
|
||||
1.145 3804.75
|
||||
1.355 3973.85
|
||||
1.452 4037.263
|
||||
1.629 4079.538
|
||||
1.742 4142.95
|
||||
1.903 4185.225
|
||||
1.935 3847.025
|
||||
2.081 3424.275
|
||||
2.129 2959.25
|
||||
2.177 2536.5
|
||||
2.194 2113.75
|
||||
2.226 1691
|
||||
2.274 1268.25
|
||||
2.323 845.5
|
||||
2.403 422.75
|
||||
2.5 0
|
||||
35
datafiles/thrustcurves/AMW_N2020.eng
Normal file
35
datafiles/thrustcurves/AMW_N2020.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;Animal Motor Works 98-11000
|
||||
N2020WT 98 870 0 5.1609 9.9693 AMW
|
||||
.106 1941.344
|
||||
0.221 2151.149
|
||||
0.381 2253.406
|
||||
0.541 2340.792
|
||||
0.701 2400.847
|
||||
0.861 2453.821
|
||||
1.021 2506.314
|
||||
1.181 2556.306
|
||||
1.341 2607.251
|
||||
1.500 2652.790
|
||||
1.660 2688.660
|
||||
1.820 2710.675
|
||||
1.980 2729.797
|
||||
2.140 2733.895
|
||||
2.300 2704.255
|
||||
2.460 2634.582
|
||||
2.620 2532.160
|
||||
2.780 2433.380
|
||||
2.940 2329.740
|
||||
3.099 2234.246
|
||||
3.259 2165.804
|
||||
3.419 2099.684
|
||||
3.579 2028.350
|
||||
3.739 1951.013
|
||||
3.899 1871.316
|
||||
4.059 1558.113
|
||||
4.219 1053.376
|
||||
4.379 890.506
|
||||
4.539 636.689
|
||||
4.998 0.000
|
||||
|
||||
;
|
||||
26
datafiles/thrustcurves/AMW_N2600.eng
Normal file
26
datafiles/thrustcurves/AMW_N2600.eng
Normal file
@ -0,0 +1,26 @@
|
||||
;
|
||||
;Animal Motor Works 98-11000
|
||||
N2600GG 98 870 1000 4.8812 10.4726 Animal_Motor_Works
|
||||
0.024 1674.37
|
||||
0.064 1949.62
|
||||
0.104 2039.52
|
||||
0.306 2189.98
|
||||
0.508 2334.45
|
||||
0.709 2491.23
|
||||
0.911 2668.93
|
||||
1.113 2874.7
|
||||
1.314 3038.83
|
||||
1.516 3191.29
|
||||
1.718 3266.01
|
||||
1.92 3318.98
|
||||
2.121 3336.18
|
||||
2.323 3229.26
|
||||
2.525 3089.68
|
||||
2.726 2943.98
|
||||
2.928 2847.69
|
||||
3.13 2751.68
|
||||
3.331 2682.22
|
||||
3.533 2463.48
|
||||
3.735 1339.63
|
||||
3.937 269.834
|
||||
4.034 0
|
||||
26
datafiles/thrustcurves/AMW_N2700.eng
Normal file
26
datafiles/thrustcurves/AMW_N2700.eng
Normal file
@ -0,0 +1,26 @@
|
||||
;
|
||||
;Animal Motor Works 98-11000
|
||||
N2700BB 98 870 1000 4.7837 9.9308 Animal_Motor_Works
|
||||
0.027 2229.53
|
||||
0.069 2476.18
|
||||
0.111 2539.74
|
||||
0.36 2723.21
|
||||
0.527 2863.83
|
||||
0.735 3016.48
|
||||
0.943 3141.25
|
||||
1.151 3241.72
|
||||
1.359 3335.56
|
||||
1.567 3519.92
|
||||
1.775 3425.88
|
||||
1.983 3420.56
|
||||
2.191 3356.08
|
||||
2.399 3270.48
|
||||
2.607 3182.6
|
||||
2.815 3098.31
|
||||
3.023 3002.95
|
||||
3.231 2888.73
|
||||
3.439 2266.61
|
||||
3.647 1498.26
|
||||
3.855 780.04
|
||||
4.063 233.545
|
||||
4.16 0
|
||||
35
datafiles/thrustcurves/AMW_N2800.eng
Normal file
35
datafiles/thrustcurves/AMW_N2800.eng
Normal file
@ -0,0 +1,35 @@
|
||||
; @File: N2800b.txt, @Pts-I: 5383, @Pts-O: 31, @Sm: 8, @CO: 5%
|
||||
; @TI: 14810.26, @TIa: 14792.71, @TIe: 0.0%, @ThMax: 3650.74, @ThAvg: 2770.17, @Tb: 5.34
|
||||
; Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar
|
||||
N2800 98 1213 100 7.6947 13.8 AMW
|
||||
0.0 93.0947
|
||||
0.0020 168.347
|
||||
0.0060 387.836
|
||||
0.019 1271.166
|
||||
0.029 1776.342
|
||||
0.043 2298.6
|
||||
0.062 2841.03
|
||||
0.072 3021.31
|
||||
0.084 3128.89
|
||||
0.14 3296.17
|
||||
0.277 3483.35
|
||||
0.293 3431.67
|
||||
0.369 3495.76
|
||||
0.978 3598.65
|
||||
1.973 3655.16
|
||||
2.977 3534.8
|
||||
3.3 3437.12
|
||||
3.497 3308.46
|
||||
3.583 3193.8
|
||||
3.651 3015.65
|
||||
3.748 2548.37
|
||||
3.836 2223.91
|
||||
4.109 1644.077
|
||||
4.245 1443.685
|
||||
4.272 1447.012
|
||||
4.397 1163.584
|
||||
4.489 1022.953
|
||||
4.516 1057.203
|
||||
4.574 883.885
|
||||
4.647 776.407
|
||||
5.569 0.0
|
||||
28
datafiles/thrustcurves/AMW_N4000.eng
Normal file
28
datafiles/thrustcurves/AMW_N4000.eng
Normal file
@ -0,0 +1,28 @@
|
||||
;
|
||||
;Animal Motor Works 98-17500
|
||||
N4000BB 98 1213 0 6.1026 13.6683 AMW
|
||||
0.029 4207.591
|
||||
0.071 4709.549
|
||||
0.113 4906.310
|
||||
0.155 5007.780
|
||||
0.239 5041.557
|
||||
0.323 4993.595
|
||||
0.534 5046.912
|
||||
0.744 5145.819
|
||||
0.954 5248.063
|
||||
1.165 5293.196
|
||||
1.375 5232.456
|
||||
1.585 5209.528
|
||||
1.796 5165.473
|
||||
2.006 5047.698
|
||||
2.216 4913.086
|
||||
2.427 4783.447
|
||||
2.637 4659.163
|
||||
2.847 4195.994
|
||||
3.058 2850.731
|
||||
3.268 1981.973
|
||||
3.478 1295.536
|
||||
3.689 907.699
|
||||
3.899 490.196
|
||||
4.110 316.338
|
||||
4.207 0.000
|
||||
40
datafiles/thrustcurves/AeroTech_D13.eng
Normal file
40
datafiles/thrustcurves/AeroTech_D13.eng
Normal file
@ -0,0 +1,40 @@
|
||||
; Aerotech D13 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
D13W 18 70 4-7-10 0.0098 0.0326 AT
|
||||
0.030 13.462
|
||||
0.061 21.171
|
||||
0.085 20.618
|
||||
0.127 21.605
|
||||
0.158 21.042
|
||||
0.182 22.306
|
||||
0.217 22.592
|
||||
0.227 23.610
|
||||
0.248 21.891
|
||||
0.279 23.155
|
||||
0.317 22.039
|
||||
0.366 21.338
|
||||
0.383 21.901
|
||||
0.449 20.648
|
||||
0.462 21.486
|
||||
0.480 19.947
|
||||
0.507 19.947
|
||||
0.521 20.509
|
||||
0.559 18.693
|
||||
0.580 19.118
|
||||
0.660 17.578
|
||||
0.743 15.337
|
||||
0.861 12.406
|
||||
0.947 9.329
|
||||
1.068 5.834
|
||||
1.155 4.158
|
||||
1.172 4.720
|
||||
1.231 2.762
|
||||
1.328 1.928
|
||||
1.404 1.093
|
||||
1.520 0.000
|
||||
26
datafiles/thrustcurves/AeroTech_D15.eng
Normal file
26
datafiles/thrustcurves/AeroTech_D15.eng
Normal file
@ -0,0 +1,26 @@
|
||||
; Aerotech D15 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
D15T 24 70 4-6-8 .0089 .0440 AT
|
||||
0.014 11.480
|
||||
0.049 26.272
|
||||
0.081 30.087
|
||||
0.107 31.261
|
||||
0.121 31.249
|
||||
0.159 31.360
|
||||
0.208 31.249
|
||||
0.283 29.583
|
||||
0.439 23.353
|
||||
0.551 18.484
|
||||
0.675 13.430
|
||||
0.863 6.422
|
||||
0.938 3.892
|
||||
1.010 2.335
|
||||
1.085 0.778
|
||||
1.142 0.389
|
||||
1.150 0.000
|
||||
33
datafiles/thrustcurves/AeroTech_D21.eng
Normal file
33
datafiles/thrustcurves/AeroTech_D21.eng
Normal file
@ -0,0 +1,33 @@
|
||||
;Aerotech D21 RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
D21T 18 70 4-7 0.0096 0.025 AT
|
||||
0.01 1.367
|
||||
0.021 19.367
|
||||
0.029 32.12
|
||||
0.037 31.667
|
||||
0.051 30.528
|
||||
0.094 30.074
|
||||
0.115 31.213
|
||||
0.133 30.074
|
||||
0.177 30.76
|
||||
0.189 29.842
|
||||
0.203 30.528
|
||||
0.226 29.842
|
||||
0.275 28.935
|
||||
0.296 29.389
|
||||
0.331 28.027
|
||||
0.421 25.971
|
||||
0.478 24.146
|
||||
0.579 20.728
|
||||
0.659 17.774
|
||||
0.739 14.356
|
||||
0.799 9.569
|
||||
0.852 4.557
|
||||
0.899 1.139
|
||||
0.94 0
|
||||
48
datafiles/thrustcurves/AeroTech_D24.eng
Normal file
48
datafiles/thrustcurves/AeroTech_D24.eng
Normal file
@ -0,0 +1,48 @@
|
||||
; AeroTech D24T (Blue Thunder) RASP.ENG file made from
|
||||
; manufacturers published data.
|
||||
;
|
||||
; File was produced May 07, 2004 by Stanley_Hemphill@Hotmail.com.
|
||||
;
|
||||
; The motor is listed in the www.thrustcurve.org database as an
|
||||
; engine certified by NAR, but there is "no data" at the weblink
|
||||
; to the NAR file database.
|
||||
;
|
||||
; The author has created this file by extracting the manufacturers
|
||||
; Thrust-Time curve from The AeroTech-2002 Catalog, and then deploting
|
||||
; 32 points using the distance measuring tools in Paint Shop Pro 8.
|
||||
; The file was then created in RockSim 7 and the motor and static values
|
||||
; were read from the RockSim Engine Editor.
|
||||
;
|
||||
; Motor Dia Len Delay Propellant Total Manufacturer
|
||||
D24BT_CO_SU 18.00 70.00 4-7-10 0.00870 0.03200 AeroTech
|
||||
0.0380 39.6000
|
||||
0.0550 36.5000
|
||||
0.0760 34.4000
|
||||
0.1220 32.4000
|
||||
0.1640 31.1000
|
||||
0.2190 30.3000
|
||||
0.2610 29.3000
|
||||
0.3080 28.7000
|
||||
0.3290 27.9000
|
||||
0.3580 26.9000
|
||||
0.3920 25.8000
|
||||
0.4340 25.0000
|
||||
0.4850 24.0000
|
||||
0.5390 23.2000
|
||||
0.5770 22.3000
|
||||
0.6200 20.9000
|
||||
0.6660 19.6000
|
||||
0.6950 18.0000
|
||||
0.7210 16.5000
|
||||
0.7500 15.5000
|
||||
0.7540 14.3000
|
||||
0.7590 12.4000
|
||||
0.7600 11.0000
|
||||
0.7630 09.1000
|
||||
0.7634 07.5000
|
||||
0.7710 05.9000
|
||||
0.7920 04.0000
|
||||
0.8300 02.6000
|
||||
0.8680 01.8000
|
||||
0.9000 01.1000
|
||||
0.9400 00.0000
|
||||
23
datafiles/thrustcurves/AeroTech_D7.eng
Normal file
23
datafiles/thrustcurves/AeroTech_D7.eng
Normal file
@ -0,0 +1,23 @@
|
||||
;Aerotech D7 RASP.ENG file made from NAR published data
|
||||
D7 24 70 100 0.0105 0.0422 AT
|
||||
0.036 3.336
|
||||
0.084 9.326
|
||||
0.101 10.281
|
||||
0.143 10.827
|
||||
0.213 10.99
|
||||
0.271 10.887
|
||||
0.359 10.685
|
||||
0.471 10.13
|
||||
0.506 10.342
|
||||
0.535 9.929
|
||||
0.81 8.697
|
||||
1.226 6.713
|
||||
1.589 5.138
|
||||
1.8 4.861
|
||||
2.151 4.581
|
||||
2.649 4.57
|
||||
2.696 3.887
|
||||
2.748 2.388
|
||||
2.807 0.889
|
||||
2.842 0.207
|
||||
2.87 0
|
||||
23
datafiles/thrustcurves/AeroTech_D9.eng
Normal file
23
datafiles/thrustcurves/AeroTech_D9.eng
Normal file
@ -0,0 +1,23 @@
|
||||
; Aerotech D9 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
D9W 24 70 4-7 0.0101 0.045 AT
|
||||
0.1 13.7
|
||||
0.15 15.4
|
||||
0.2 16.3
|
||||
0.25 16.8
|
||||
0.35 17.2
|
||||
0.40 17.2
|
||||
0.50 16.8
|
||||
0.65 15.9
|
||||
0.80 14.5
|
||||
1.10 9.2
|
||||
1.25 7.0
|
||||
1.40 4.8
|
||||
1.60 2.5
|
||||
1.90 0.0
|
||||
13
datafiles/thrustcurves/AeroTech_E11.eng
Normal file
13
datafiles/thrustcurves/AeroTech_E11.eng
Normal file
@ -0,0 +1,13 @@
|
||||
;
|
||||
;Based On NAR Test Data
|
||||
;12/23/93
|
||||
E11J 24 70 4 0.025 0.0624 Aerotech
|
||||
0.0725446 14.3704
|
||||
0.16183 17.6296
|
||||
0.206473 18.3704
|
||||
0.418527 19.2593
|
||||
0.731027 18.3704
|
||||
1.31696 14.2222
|
||||
1.91964 9.03704
|
||||
2.51116 2.22222
|
||||
2.83 0
|
||||
42
datafiles/thrustcurves/AeroTech_E12.eng
Normal file
42
datafiles/thrustcurves/AeroTech_E12.eng
Normal file
@ -0,0 +1,42 @@
|
||||
;
|
||||
;
|
||||
;Aerotech E12JRC RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
E12JRC 24 70 100 0.0303 0.0594 AT
|
||||
0.054 16.764
|
||||
0.095 18.33
|
||||
0.197 16.545
|
||||
0.313 16.654
|
||||
0.36 17.211
|
||||
0.401 16.316
|
||||
0.442 17.55
|
||||
0.476 16.206
|
||||
0.578 16.316
|
||||
0.666 16.764
|
||||
0.7 15.649
|
||||
0.768 16.316
|
||||
0.89 16.097
|
||||
1.019 15.649
|
||||
1.162 14.983
|
||||
1.23 14.983
|
||||
1.25 13.968
|
||||
1.291 14.754
|
||||
1.332 13.749
|
||||
1.373 14.197
|
||||
1.434 13.53
|
||||
1.488 13.749
|
||||
1.597 12.635
|
||||
1.726 11.401
|
||||
1.828 10.615
|
||||
1.889 9.613
|
||||
1.957 9.613
|
||||
1.998 8.495
|
||||
2.093 8.607
|
||||
2.277 7.042
|
||||
2.487 5.813
|
||||
3.05 0
|
||||
46
datafiles/thrustcurves/AeroTech_E15.eng
Normal file
46
datafiles/thrustcurves/AeroTech_E15.eng
Normal file
@ -0,0 +1,46 @@
|
||||
; E15W-4,7,P from NAR data
|
||||
E15W 24 70 4-7-P 0.020100000000000003 0.0502 AT
|
||||
0.012 9.918
|
||||
0.018 20.205
|
||||
0.027 25.257
|
||||
0.039 28.152
|
||||
0.055 28.768
|
||||
0.088 27.29
|
||||
0.197 24.517
|
||||
0.297 22.977
|
||||
0.467 20.945
|
||||
0.561 19.959
|
||||
0.679 20.021
|
||||
0.722 19.22
|
||||
0.761 18.789
|
||||
0.807 20.021
|
||||
0.84 18.234
|
||||
0.904 18.727
|
||||
0.995 17.926
|
||||
1.034 18.172
|
||||
1.104 16.756
|
||||
1.147 17.248
|
||||
1.256 16.386
|
||||
1.377 15.77
|
||||
1.411 14.846
|
||||
1.426 16.324
|
||||
1.45 15.031
|
||||
1.547 14.353
|
||||
1.559 16.016
|
||||
1.589 13.86
|
||||
1.62 14.23
|
||||
1.693 13.121
|
||||
1.72 13.429
|
||||
1.829 12.936
|
||||
1.866 11.951
|
||||
1.944 11.951
|
||||
2.005 10.965
|
||||
2.093 10.472
|
||||
2.236 8.316
|
||||
2.26 9.055
|
||||
2.278 7.207
|
||||
2.378 4.99
|
||||
2.442 2.71
|
||||
2.499 1.602
|
||||
2.548 1.047
|
||||
2.618 0.0
|
||||
41
datafiles/thrustcurves/AeroTech_E15_1.eng
Normal file
41
datafiles/thrustcurves/AeroTech_E15_1.eng
Normal file
@ -0,0 +1,41 @@
|
||||
; Aerotech E15 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
E15W 24 70 4-7 .0201 .0501 AT
|
||||
0.020 23.330
|
||||
0.036 27.318
|
||||
0.058 28.840
|
||||
0.079 27.171
|
||||
0.139 25.638
|
||||
0.183 24.263
|
||||
0.237 24.106
|
||||
0.297 22.426
|
||||
0.373 21.964
|
||||
0.400 20.894
|
||||
0.443 21.355
|
||||
0.487 20.442
|
||||
0.617 19.833
|
||||
0.742 18.457
|
||||
0.812 20.000
|
||||
0.850 18.006
|
||||
0.899 18.467
|
||||
1.035 17.711
|
||||
1.100 16.945
|
||||
1.160 16.945
|
||||
1.377 15.736
|
||||
1.426 14.656
|
||||
1.436 16.198
|
||||
1.463 14.813
|
||||
1.550 14.361
|
||||
1.572 15.432
|
||||
1.610 13.752
|
||||
1.827 12.839
|
||||
2.126 10.098
|
||||
2.337 6.116
|
||||
2.538 1.369
|
||||
2.600 0.000
|
||||
32
datafiles/thrustcurves/AeroTech_E16.eng
Normal file
32
datafiles/thrustcurves/AeroTech_E16.eng
Normal file
@ -0,0 +1,32 @@
|
||||
; Aerotech E16 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
E16W 29 124 4-7-10 .0190 .107 AT
|
||||
0.132 32.223
|
||||
0.221 37.200
|
||||
0.255 36.699
|
||||
0.306 36.699
|
||||
0.371 35.357
|
||||
0.414 33.785
|
||||
0.437 34.906
|
||||
0.472 33.785
|
||||
0.530 32.894
|
||||
0.553 31.772
|
||||
0.576 32.443
|
||||
0.638 29.309
|
||||
0.720 27.296
|
||||
0.867 23.942
|
||||
1.083 19.245
|
||||
1.273 14.319
|
||||
1.458 9.397
|
||||
1.513 8.055
|
||||
1.524 8.279
|
||||
1.555 6.936
|
||||
1.656 4.474
|
||||
1.814 1.790
|
||||
2.000 0.000
|
||||
37
datafiles/thrustcurves/AeroTech_E18.eng
Normal file
37
datafiles/thrustcurves/AeroTech_E18.eng
Normal file
@ -0,0 +1,37 @@
|
||||
; Aerotech E18 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
E18W 24 70 4-8-10 .0207 .057 AT
|
||||
0.016 6.586
|
||||
0.042 18.004
|
||||
0.073 27.138
|
||||
0.098 29.815
|
||||
0.134 30.357
|
||||
0.170 30.347
|
||||
0.195 31.080
|
||||
0.236 30.347
|
||||
0.287 30.878
|
||||
0.338 30.337
|
||||
0.368 30.878
|
||||
0.404 29.795
|
||||
0.424 30.688
|
||||
0.465 29.976
|
||||
0.526 29.785
|
||||
0.592 29.063
|
||||
0.669 28.341
|
||||
0.786 26.908
|
||||
0.908 23.850
|
||||
1.025 21.163
|
||||
1.157 17.905
|
||||
1.284 14.857
|
||||
1.462 11.338
|
||||
1.660 7.106
|
||||
1.838 3.470
|
||||
2.006 1.309
|
||||
2.083 0.588
|
||||
2.140 0.000
|
||||
30
datafiles/thrustcurves/AeroTech_E23.eng
Normal file
30
datafiles/thrustcurves/AeroTech_E23.eng
Normal file
@ -0,0 +1,30 @@
|
||||
; Aerotech E23 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
E23T 29 124 5-8 .0174 .1039 AT
|
||||
0.024 16.299
|
||||
0.035 21.959
|
||||
0.067 30.785
|
||||
0.090 35.774
|
||||
0.153 37.577
|
||||
0.200 38.220
|
||||
0.240 37.357
|
||||
0.322 37.577
|
||||
0.393 35.093
|
||||
0.534 32.378
|
||||
0.727 27.168
|
||||
0.766 26.938
|
||||
0.798 25.125
|
||||
0.908 21.729
|
||||
1.057 16.980
|
||||
1.187 12.682
|
||||
1.336 7.471
|
||||
1.450 3.169
|
||||
1.497 1.584
|
||||
1.532 0.679
|
||||
1.570 0.000
|
||||
36
datafiles/thrustcurves/AeroTech_E28.eng
Normal file
36
datafiles/thrustcurves/AeroTech_E28.eng
Normal file
@ -0,0 +1,36 @@
|
||||
; Aerotech E28 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
E28T 24 70 2-5-8 .0184 .0545 A
|
||||
0.010 29.8620
|
||||
0.018 45.1390
|
||||
0.038 47.5620
|
||||
0.081 50.5200
|
||||
0.106 48.9530
|
||||
0.146 48.2630
|
||||
0.161 48.9530
|
||||
0.197 48.9530
|
||||
0.242 47.5620
|
||||
0.313 46.1800
|
||||
0.411 43.0570
|
||||
0.494 40.6240
|
||||
0.527 39.5830
|
||||
0.542 40.2740
|
||||
0.562 38.5420
|
||||
0.633 36.4600
|
||||
0.683 34.3770
|
||||
0.743 31.2440
|
||||
0.799 29.1620
|
||||
0.877 26.0380
|
||||
0.970 20.8320
|
||||
1.006 17.3590
|
||||
1.046 11.4620
|
||||
1.089 6.9430
|
||||
1.132 3.8190
|
||||
1.172 1.7350
|
||||
1.220 0.0000
|
||||
34
datafiles/thrustcurves/AeroTech_E30.eng
Normal file
34
datafiles/thrustcurves/AeroTech_E30.eng
Normal file
@ -0,0 +1,34 @@
|
||||
; Aerotech E30 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
E30T 24 70 4-7 .0193 .0433 AT
|
||||
0.013 38.8470
|
||||
0.020 45.6210
|
||||
0.041 48.2700
|
||||
0.059 46.5020
|
||||
0.110 46.5020
|
||||
0.166 45.9120
|
||||
0.184 46.7920
|
||||
0.217 45.9120
|
||||
0.265 45.9120
|
||||
0.319 45.0310
|
||||
0.383 44.1500
|
||||
0.482 42.0890
|
||||
0.594 38.8470
|
||||
0.615 39.4370
|
||||
0.628 37.3760
|
||||
0.684 35.3140
|
||||
0.742 33.2630
|
||||
0.804 30.0210
|
||||
0.880 25.6070
|
||||
0.962 20.0140
|
||||
1.038 12.9490
|
||||
1.089 7.3580
|
||||
1.151 3.2370
|
||||
1.186 1.1760
|
||||
1.200 0.0000
|
||||
20
datafiles/thrustcurves/AeroTech_E6.eng
Normal file
20
datafiles/thrustcurves/AeroTech_E6.eng
Normal file
@ -0,0 +1,20 @@
|
||||
; Aerotech E6T single use from NAR cert data
|
||||
E6T 24 70 2-4-8-P 0.021500000000000002 0.0463 AT
|
||||
0.011 18.085
|
||||
0.109 19.681
|
||||
0.217 16.312
|
||||
0.315 13.475
|
||||
0.457 11.348
|
||||
0.63 9.043
|
||||
0.804 7.801
|
||||
0.989 6.738
|
||||
1.272 6.028
|
||||
2.0 5.851
|
||||
3.0 5.496
|
||||
4.0 5.496
|
||||
4.446 4.965
|
||||
5.011 4.965
|
||||
5.533 4.787
|
||||
5.609 6.56
|
||||
5.707 4.255
|
||||
6.033 0.0
|
||||
34
datafiles/thrustcurves/AeroTech_E7.eng
Normal file
34
datafiles/thrustcurves/AeroTech_E7.eng
Normal file
@ -0,0 +1,34 @@
|
||||
;
|
||||
;Aerotech E7TRC RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
E7RC 24 70 100 0.0171 0.0484 AT
|
||||
0.038 6.636
|
||||
0.063 10.056
|
||||
0.087 11.019
|
||||
0.134 11.42
|
||||
0.206 11.58
|
||||
0.312 11.149
|
||||
0.466 10.738
|
||||
0.667 9.777
|
||||
0.94 8.132
|
||||
1.223 6.281
|
||||
1.484 5.182
|
||||
1.709 4.701
|
||||
2.112 4.423
|
||||
2.776 4.279
|
||||
3.31 4.205
|
||||
3.926 4.266
|
||||
4.401 4.192
|
||||
4.638 4.258
|
||||
4.744 4.119
|
||||
5.124 3.979
|
||||
5.219 3.977
|
||||
5.266 3.156
|
||||
5.313 1.992
|
||||
5.36 0.965
|
||||
5.43 0
|
||||
30
datafiles/thrustcurves/AeroTech_F10.eng
Normal file
30
datafiles/thrustcurves/AeroTech_F10.eng
Normal file
@ -0,0 +1,30 @@
|
||||
;
|
||||
F10 29.0 92.00 4-6-8 0.04000 0.08300 Aerotech
|
||||
0.01 16.81
|
||||
0.03 22.34
|
||||
0.11 22.23
|
||||
0.26 21.49
|
||||
0.37 20.00
|
||||
0.47 20.21
|
||||
0.67 18.09
|
||||
0.99 15.74
|
||||
1.31 13.40
|
||||
1.81 10.85
|
||||
2.49 10.21
|
||||
3.13 8.94
|
||||
3.60 8.83
|
||||
4.11 8.62
|
||||
4.95 8.62
|
||||
5.45 8.62
|
||||
5.58 8.51
|
||||
5.88 8.72
|
||||
6.22 8.51
|
||||
6.46 8.51
|
||||
6.60 7.77
|
||||
6.71 7.02
|
||||
6.79 5.64
|
||||
6.91 3.83
|
||||
6.95 2.23
|
||||
7.00 0.96
|
||||
7.05 0.00
|
||||
;
|
||||
40
datafiles/thrustcurves/AeroTech_F12.eng
Normal file
40
datafiles/thrustcurves/AeroTech_F12.eng
Normal file
@ -0,0 +1,40 @@
|
||||
; Aerotech F12 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (4/6/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
F12J 24 70 2-5 .0303 .0667 AT
|
||||
0.037 20.894
|
||||
0.054 22.152
|
||||
0.101 22.152
|
||||
0.148 22.571
|
||||
0.165 23.409
|
||||
0.200 22.421
|
||||
0.281 22.142
|
||||
0.369 22.132
|
||||
0.474 22.271
|
||||
0.526 23.540
|
||||
0.549 21.982
|
||||
0.637 22.122
|
||||
0.724 21.842
|
||||
0.800 21.413
|
||||
0.823 22.251
|
||||
0.846 20.714
|
||||
0.881 21.553
|
||||
0.945 21.123
|
||||
1.021 20.704
|
||||
1.114 20.554
|
||||
1.213 19.296
|
||||
1.382 18.298
|
||||
1.481 18.019
|
||||
1.737 15.343
|
||||
1.790 17.300
|
||||
1.883 13.936
|
||||
2.051 11.260
|
||||
2.220 7.468
|
||||
2.447 3.671
|
||||
2.709 1.135
|
||||
2.930 0.000
|
||||
38
datafiles/thrustcurves/AeroTech_F13.eng
Normal file
38
datafiles/thrustcurves/AeroTech_F13.eng
Normal file
@ -0,0 +1,38 @@
|
||||
;
|
||||
;Aerotech F13RCJ RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
F13RCJ 32 107 100 0.0323 0.1105 AT
|
||||
0.048 15.309
|
||||
0.084 18.629
|
||||
0.143 19.98
|
||||
0.311 18.968
|
||||
0.538 18.172
|
||||
0.729 17.138
|
||||
0.992 15.428
|
||||
1.279 13.828
|
||||
1.673 12.456
|
||||
1.984 11.879
|
||||
2.044 12.227
|
||||
2.139 11.313
|
||||
2.378 11.193
|
||||
2.51 11.084
|
||||
2.558 12.108
|
||||
2.641 10.855
|
||||
2.976 10.736
|
||||
3.49 10.627
|
||||
3.873 10.507
|
||||
3.992 10.965
|
||||
4.028 10.627
|
||||
4.41 10.507
|
||||
4.625 10.736
|
||||
4.769 9.941
|
||||
4.829 8.684
|
||||
4.865 6.742
|
||||
4.96 3.199
|
||||
5.02 1.485
|
||||
5.1 0
|
||||
41
datafiles/thrustcurves/AeroTech_F16.eng
Normal file
41
datafiles/thrustcurves/AeroTech_F16.eng
Normal file
@ -0,0 +1,41 @@
|
||||
;
|
||||
;Aerotech F16RCJ RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
F16RCJ 32 107 100 0.0625 0.1404 AT
|
||||
0.046 26.35
|
||||
0.116 22.388
|
||||
0.139 21.374
|
||||
0.185 21.886
|
||||
0.22 20.54
|
||||
0.301 19.696
|
||||
0.498 18.35
|
||||
0.579 19.194
|
||||
0.637 16.492
|
||||
0.718 18.35
|
||||
0.834 18.35
|
||||
0.95 18.35
|
||||
1.054 19.194
|
||||
1.147 17.848
|
||||
1.181 18.853
|
||||
1.263 17.336
|
||||
1.436 18.009
|
||||
1.633 17.165
|
||||
1.784 17.336
|
||||
1.865 18.682
|
||||
1.934 16.834
|
||||
1.981 17.336
|
||||
2.178 16.332
|
||||
2.375 16.332
|
||||
2.502 18.18
|
||||
2.664 15.659
|
||||
2.896 15.488
|
||||
3.29 13.8
|
||||
3.718 11.611
|
||||
4.181 9.426
|
||||
4.888 5.891
|
||||
5.69 0
|
||||
35
datafiles/thrustcurves/AeroTech_F20.eng
Normal file
35
datafiles/thrustcurves/AeroTech_F20.eng
Normal file
@ -0,0 +1,35 @@
|
||||
;
|
||||
;
|
||||
F20EJ 29 83 4-7 0.03 0.0746 AeroTech
|
||||
0.01 52.08
|
||||
0.03 49.81
|
||||
0.06 46.98
|
||||
0.1 45.56
|
||||
0.15 44.49
|
||||
0.18 45.55
|
||||
0.21 43.42
|
||||
0.24 43.78
|
||||
0.32 43.77
|
||||
0.36 44.11
|
||||
0.44 43.04
|
||||
0.45 40.58
|
||||
0.53 39.86
|
||||
0.62 38.08
|
||||
0.76 36.3
|
||||
0.8 37.35
|
||||
0.84 34.88
|
||||
0.89 36.99
|
||||
0.9 33.46
|
||||
1.03 30.61
|
||||
1.06 32.02
|
||||
1.09 29.55
|
||||
1.23 26
|
||||
1.32 22.45
|
||||
1.35 23.16
|
||||
1.36 21.39
|
||||
1.58 16.42
|
||||
1.8 11.1
|
||||
2.01 6.48
|
||||
2.19 3.63
|
||||
2.39 1.13
|
||||
2.68 0
|
||||
60
datafiles/thrustcurves/AeroTech_F21.eng
Normal file
60
datafiles/thrustcurves/AeroTech_F21.eng
Normal file
@ -0,0 +1,60 @@
|
||||
; Aerotech F21W (White Lightning) RASP.ENG file.
|
||||
; File produced Jun 22 2004.
|
||||
; The file was produced by scaling data points off the
|
||||
; thrust curve in the Tripoli.org motor pdf file.
|
||||
;
|
||||
; The F21W cannot be found on thrustcurve.org.
|
||||
; Hence the amateur file production.
|
||||
; The file was created by Stan Hemphill
|
||||
; Contact at stanley_hemphill@hotmail.com
|
||||
;
|
||||
; Motor ## Dia Len Delays Prop Motor Company
|
||||
F21WL_CO_SU 24 96 6-8 0.0300 0.064 AeroTech
|
||||
0.0045 037.2266
|
||||
0.0090 042.1474
|
||||
0.0180 042.5040
|
||||
0.0270 040.5071
|
||||
0.0337 038.8669
|
||||
0.0427 038.2250
|
||||
0.0517 037.7258
|
||||
0.0607 036.8700
|
||||
0.0720 036.4422
|
||||
0.0877 036.4422
|
||||
0.1102 035.3724
|
||||
0.1350 035.8716
|
||||
0.1552 035.4437
|
||||
0.1732 036.2282
|
||||
0.2025 035.6577
|
||||
0.2452 037.2979
|
||||
0.2835 036.5848
|
||||
0.3195 038.0111
|
||||
0.3375 037.4406
|
||||
0.3757 038.5816
|
||||
0.3960 038.2250
|
||||
0.4297 039.3661
|
||||
0.4454 038.0111
|
||||
0.4747 038.7242
|
||||
0.4882 037.7971
|
||||
0.5084 038.1537
|
||||
0.5354 038.5103
|
||||
0.5647 037.9398
|
||||
0.5849 037.2266
|
||||
0.6007 037.8685
|
||||
0.6389 036.8700
|
||||
0.6704 037.1553
|
||||
0.7649 035.9429
|
||||
0.9201 032.9477
|
||||
1.0056 030.3090
|
||||
1.0709 029.7385
|
||||
1.2643 024.0333
|
||||
1.2868 024.0333
|
||||
1.3723 020.8241
|
||||
1.3926 020.8241
|
||||
1.5883 015.4754
|
||||
1.6108 015.4754
|
||||
2.0112 005.0634
|
||||
2.1192 003.4231
|
||||
2.2407 002.4247
|
||||
2.3780 001.4976
|
||||
2.4927 000.9271
|
||||
2.5152 000.0000
|
||||
38
datafiles/thrustcurves/AeroTech_F22.eng
Normal file
38
datafiles/thrustcurves/AeroTech_F22.eng
Normal file
@ -0,0 +1,38 @@
|
||||
;
|
||||
;Aerotech F22 RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
F22 29 125 4-7 0.0463 0.1342 AT
|
||||
0.014 11.527
|
||||
0.075 20.126
|
||||
0.157 26.572
|
||||
0.293 29.113
|
||||
0.382 30.278
|
||||
0.45 29.69
|
||||
0.539 30.667
|
||||
0.614 30.089
|
||||
0.662 31.15
|
||||
0.771 30.478
|
||||
0.948 29.89
|
||||
0.996 28.714
|
||||
1.078 28.136
|
||||
1.187 27.738
|
||||
1.289 26.761
|
||||
1.337 26.96
|
||||
1.412 25.984
|
||||
1.474 25.008
|
||||
1.515 26.173
|
||||
1.542 24.808
|
||||
1.706 22.856
|
||||
1.938 20.903
|
||||
2.101 18.173
|
||||
2.129 19.338
|
||||
2.251 16.21
|
||||
2.402 13.48
|
||||
2.64 8.791
|
||||
2.961 3.32
|
||||
3.31 0
|
||||
36
datafiles/thrustcurves/AeroTech_F23.eng
Normal file
36
datafiles/thrustcurves/AeroTech_F23.eng
Normal file
@ -0,0 +1,36 @@
|
||||
;
|
||||
;F23FJ Motor Thrust Curve created by Tim Van Milligan
|
||||
;for RockSim Users - www.rocksim.com
|
||||
;file produced March 2, 2005
|
||||
;Based on data supplied by Aerotech for the newer molded case F23 econojet.
|
||||
F23FJ 29 83 4-7 0.033 0.0839 AeroTech
|
||||
0.03 48.7
|
||||
0.05 43.11
|
||||
0.08 41.41
|
||||
0.1 42.26
|
||||
0.13 40.84
|
||||
0.17 39.42
|
||||
0.23 38.85
|
||||
0.27 38.85
|
||||
0.3 37.44
|
||||
0.31 38.57
|
||||
0.36 37.72
|
||||
0.43 36.59
|
||||
0.5 36.02
|
||||
0.56 36.02
|
||||
0.59 34.6
|
||||
0.69 33.18
|
||||
0.77 32.61
|
||||
0.85 31.2
|
||||
0.94 29.5
|
||||
1.04 27.79
|
||||
1.18 24.39
|
||||
1.2 25.24
|
||||
1.25 22.97
|
||||
1.37 20.98
|
||||
1.53 16.73
|
||||
1.69 12.48
|
||||
1.83 9.07
|
||||
1.95 5.11
|
||||
2.07 2.27
|
||||
2.22 0
|
||||
41
datafiles/thrustcurves/AeroTech_F23_1.eng
Normal file
41
datafiles/thrustcurves/AeroTech_F23_1.eng
Normal file
@ -0,0 +1,41 @@
|
||||
;
|
||||
;Aerotech F23RCWSK RASP.ENG file made from NAR published data
|
||||
;File produced July 4, 2000
|
||||
;The total impulse, peak thrust, average thrust and burn time are
|
||||
;the same as the averaged static test data on the NAR web site in
|
||||
;the certification file. The curve drawn with these data points is as
|
||||
;close to the certification curve as can be with such a limited
|
||||
;number of points (32) allowed with wRASP up to v1.6.
|
||||
F23-RC-SK 32 107 100 0.0378 0.1287 AT
|
||||
0.042 22.644
|
||||
0.133 28.191
|
||||
0.161 27.261
|
||||
0.189 29.57
|
||||
0.252 31.419
|
||||
0.343 32.578
|
||||
0.399 32.348
|
||||
0.441 33.737
|
||||
0.476 30.729
|
||||
0.539 33.507
|
||||
0.609 34.197
|
||||
0.777 34.886
|
||||
0.826 34.656
|
||||
0.896 36
|
||||
0.938 34.656
|
||||
1.015 34.656
|
||||
1.071 34.197
|
||||
1.12 33.038
|
||||
1.218 32.578
|
||||
1.267 29.81
|
||||
1.351 29.34
|
||||
1.393 27.731
|
||||
1.54 26.802
|
||||
1.645 24.263
|
||||
1.799 21.255
|
||||
1.862 19.866
|
||||
2.051 15.479
|
||||
2.317 11.552
|
||||
2.618 6.7
|
||||
2.884 3.234
|
||||
3.185 1.386
|
||||
3.47 0
|
||||
34
datafiles/thrustcurves/AeroTech_F24.eng
Normal file
34
datafiles/thrustcurves/AeroTech_F24.eng
Normal file
@ -0,0 +1,34 @@
|
||||
; Aerotech F24 RASP.ENG file made from NAR published data
|
||||
; File produced July 4, 2000
|
||||
; Submitted to ThrustCurve.org by Chris Kobel (4/6/07)
|
||||
; The total impulse, peak thrust, average thrust and burn time are
|
||||
; the same as the averaged static test data on the NAR web site in
|
||||
; the certification file. The curve drawn with these data points is as
|
||||
; close to the certification curve as can be with such a limited
|
||||
; number of points (32) allowed with wRASP up to v1.6.
|
||||
F24W 24 70 4-7-10 .0253 .062 AT
|
||||
0.033 16.442
|
||||
0.112 40.646
|
||||
0.125 41.450
|
||||
0.180 40.927
|
||||
0.245 40.626
|
||||
0.281 41.017
|
||||
0.355 40.024
|
||||
0.438 39.713
|
||||
0.543 38.227
|
||||
0.603 37.032
|
||||
0.658 33.779
|
||||
0.685 34.663
|
||||
0.726 29.934
|
||||
0.772 30.216
|
||||
0.951 26.953
|
||||
1.071 25.166
|
||||
1.107 23.088
|
||||
1.185 21.311
|
||||
1.383 17.144
|
||||
1.649 10.910
|
||||
1.828 5.869
|
||||
1.938 2.903
|
||||
1.988 2.306
|
||||
2.048 1.412
|
||||
2.130 0.000
|
||||
15
datafiles/thrustcurves/AeroTech_F25.eng
Normal file
15
datafiles/thrustcurves/AeroTech_F25.eng
Normal file
@ -0,0 +1,15 @@
|
||||
;
|
||||
;F25 Motor Thrust Curve created by Tim Van Milligan
|
||||
;for RockSim Users - www.rocksim.com
|
||||
;file produced March 2, 2005
|
||||
;Based on data supplied by Aerotech for the newer molded case F25.
|
||||
F25 29 98 4-6-9 0.0388 0.0972 Aerotech
|
||||
0.039 57.631
|
||||
0.187 53.491
|
||||
0.342 51.239
|
||||
0.5 47.86
|
||||
1 33.806
|
||||
1.5 22.94
|
||||
2 10.135
|
||||
2.207 4.504
|
||||
2.69 0
|
||||
20
datafiles/thrustcurves/AeroTech_F26.eng
Normal file
20
datafiles/thrustcurves/AeroTech_F26.eng
Normal file
@ -0,0 +1,20 @@
|
||||
;
|
||||
;F26FJ Motor Thrust Curve created by Tim Van Milligan
|
||||
;for RockSim Users - www.rocksim.com
|
||||
;File created March 2, 2005
|
||||
;Based on data supplied by Aerotech prior to NAR certification.
|
||||
F26FJ 29 98 6-9 0.0431 0.1007 Aerotech
|
||||
0.041 38.289
|
||||
0.114 36.318
|
||||
0.293 34.347
|
||||
0.497 32.939
|
||||
0.774 32.376
|
||||
1 31.25
|
||||
1.254 28.716
|
||||
1.498 25.338
|
||||
1.743 22.241
|
||||
2.003 17.737
|
||||
2.077 15.484
|
||||
2.304 5.349
|
||||
2.484 1.689
|
||||
2.61 0
|
||||
36
datafiles/thrustcurves/AeroTech_F27.eng
Normal file
36
datafiles/thrustcurves/AeroTech_F27.eng
Normal file
@ -0,0 +1,36 @@
|
||||
; Exported using ThrustCurveTool, www.ThrustGear.com
|
||||
; @File: 060603WF27Composite.txt, @Pts-I: 1001, @Pts-O: 32, @Sm: 5, @CO: 5%
|
||||
; @TI: 49.5446, @TIa: 49.299, @TIe: 0.0%, @ThMax: 36.2491, @ThAvg: 24.1799, @Tb: 2.049
|
||||
F27 29 83 4,8 0.0284 0.08 Aerotech
|
||||
0.0 4.84718
|
||||
0.0125 15.5374
|
||||
0.0175 18.81827
|
||||
0.025 22.5311
|
||||
0.0325 25.2547
|
||||
0.04 27.3204
|
||||
0.0575 30.3657
|
||||
0.0725 31.4597
|
||||
0.0975 32.2507
|
||||
0.265 35.0238
|
||||
0.295 35.9203
|
||||
0.4675 35.9684
|
||||
0.59 35.065
|
||||
0.8 32.0145
|
||||
0.825 31.2773
|
||||
0.8575 31.1102
|
||||
0.9025 29.9308
|
||||
0.955 29.7244
|
||||
1.045 27.2951
|
||||
1.085 27.2663
|
||||
1.1175 25.9881
|
||||
1.1475 26.0014
|
||||
1.235 23.2853
|
||||
1.28 22.9001
|
||||
1.3425 21.0771
|
||||
1.52 17.256
|
||||
1.8075 6.85478
|
||||
1.9175 4.16387
|
||||
2.05 1.783863
|
||||
2.1775 0.488016
|
||||
2.4225 0.44385
|
||||
2.425 0.0
|
||||
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Reference in New Issue
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