JoePfeiffer f8430c6504 Calculate fintab height from body radii at for and aft fintab extents, instead ...

of assuming constant radius body tube

2020-12-12 19:13:08 -07:00

..

.settings

[upgrade] Updated Eclipse buildfiles to use Java 1.8

2018-06-17 15:34:55 -04:00

lib

[rm] remove duplicate jogl jar

2020-07-19 16:05:24 -04:00

reference

Update to MigLayout 4.0.

2013-11-11 09:51:53 -06:00

resources/datafiles

[fix][example] Fixes 'High Power Airstart' -- with new motor: I211

2020-03-30 20:21:15 -04:00

resources-src/datafiles

Upon further research the estes nc data contained incorrect PNC-80FB

2014-04-23 15:15:38 -05:00

src/net/sf/openrocket

Calculate fintab height from body radii at for and aft fintab extents, instead

2020-12-12 19:13:08 -07:00

test/net/sf/openrocket

The deleted methods (setTotalThrustEstimate(), setBurnTimeEstimate(), setAverageThrustEstimate(), and setMaxThrustEstimate()) were never called. The member variables maxThrust, burnTimeEstimate, averageThrust, totalImpulse are all calculated by computeStatistics() and the values (if any) from the thrustcurve file are ignored.

2020-04-22 09:29:57 -06:00

.classpath

Adjust IntelliJ and Eclipse classpaths to new guice

2020-04-02 19:22:42 -07:00

.gitignore

…

.project

…

build.xml

Update guice library to remove AOP; Fixes issue #609

2020-04-02 15:56:55 -07:00

OpenRocket Swing.iml

Adjust .iml files for IntelliJ

2020-04-05 12:36:07 -07:00