2009-05-31 17:23:49 +00:00
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< title > OpenRocket— Features< / title >
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< h1 > Features of OpenRocket< / h1 >
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< li > OpenRocket< / li >
< li > < a href = "index.html" > Home< / a > < / li >
< li > < a href = "features.html" > Features< / a > < / li >
< li > < a href = "screenshots.html" > Screenshots< / a > < / li >
< li > < a href = "download.html" > Download< / a > < / li >
< li > < a href = "documentation.html" > Documentation< / a > < / li >
< li > < a href = "contact.html" >
Mailing lists< br / >
Support forums< br / >
Contact info< / a > < / li >
< li > < a href = "report.html" >
Report a bug< br / >
Request a feature< / a > < / li >
< li > < a href = "license.html" > License< / a > < / li >
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< h2 > Current features< / h2 >
< h3 > General< / h3 >
< ul >
< li > < strong > Fully cross-platform< / strong > , written in Java< / li >
< li > < strong > Fully documented< / strong > < a href = "documentation.html" > simulation
methods< / a > < / li >
< li > < strong > Open Source< / strong > , source code available under the
< a href = "license.html" > GNU GPL< / a > < / li >
< / ul >
< h3 > User interface< / h3 >
< ul >
< li > < a href = "screenshots.html" > Easy-to-use user interface< / a > for
rocket design< / li >
< li > < strong > Zoomable schematic view< / strong > of rocket from the side or rear< / li >
< li > Rocket rotation around center axis< / li >
< li > < strong > Real-time view of CG and CP< / strong > position< / li >
< li > < strong > Real-time flight altitude, velocity and
acceleration< / strong > information from a continuous simulation
performed in the background< / li >
< / ul >
< h3 > Design< / h3 >
< ul >
< li > A multitude of available components to
choose from< / li >
< li > < strong > Trapezoidal< / strong > , < strong > elliptical< / strong >
and < strong > free-form fins< / strong > supported< / li >
< li > Support for < strong > canted fins< / strong > (roll
stabilization)< / li >
< li > < strong > Staging< / strong > and < strong > clustering< / strong > support< / li >
< li > Automatic calculation of component mass and CG based on
shape and density< / li >
< li > Ability to < strong > override mass and CG< / strong > of
components or stages separately< / li >
< / ul >
< h3 > Simulation and analysis< / h3 >
< ul >
< li > Full < strong > six degree of freedom< / strong > simulation< / li >
< li > Rocket stability computed using < strong > extended Barrowman
method< / strong > < / li >
< li > Realistic wind modeling< / li >
< li > Analysis of the < strong > effect of separate
components< / strong > on the stability, drag and roll
characteristics of the rocket< / li >
< li > < strong > Fully configurable plotting< / strong > , with
various preset configurations< / li >
< li > < strong > Simulation listeners< / strong > allowing custom-made
code to interact with the rocket during flight simulation< / li >
< / ul >
< h2 id = "future" > Planned future features< / h2 >
< p > OpenRocket is under constant work, and anybody can help make
OpenRocket an even better simulator! Here are a few features that
have been planned...< / p >
< ul >
< li > Aerodynamic computation using
< acronym title = "Computational Fluid Dynamics" > CFD< / acronym >
< a href = "contact.html" class = "help" > (help needed!)< / a > < / li >
< li > Better support for supersonic simulation
< a href = "contact.html" class = "help" > (help needed!)< / a > < / li >
< li > 3D view of the rocket design
< a href = "contact.html" class = "help" > (help needed!)< / a > < / li >
< li > Saving figures and exporting simulation data< / li >
< li > Importing and plotting actual flight data from altimeters< / li >
< li > Importing new motor thrust curves< / li >
< li > Support for ready-made component databases< / li >
< li > Customized support for hybrid rocket motors and water
rockets< / li >
< li > Rocket flight animation< / li >
< li > A "wizard" for creating new rocket designs< / li >
< li > . . .< / li >
< / ul >
< p > If you want to help make OpenRocket the best rocket simulator,
don't hesitate to < a href = "contact.html" > contact us< / a > !< / p >
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