CRP LOGO
COMPUTER SOFTWARE - IBM, MAC, SOURCE
by Jerry Irvine
ITEM #ISBN #TITLEDESCRIPTIONCost
SUB0-912468-12-2Subsonic Altitude PredictionIncludes Center of Pressure
and Coefficient of Drag
For use with subsonic model and consumer rockets.
Closed form solution.
Download of BASIC source.
$80.00
SUPER0-912468-13-0Supersonic Altitude PredictionIncludes Center of Pressure
and Coefficient of Drag
For use with all but the highest performance rockets.
Runge-Kutta solution.
Supports multi-stage, multi-motor, custom motor.
Download of BASIC source.
$180.00
SORB0-912468-14-9Hypersonic Altitude PredictionIncludes CP, CD, Trajectory.
For use with anything short of orbital insertion.
Runge-Kutta solution.
Supports multi-stage, multi-motor, custom motor.
Download of BASIC source.
$280.00
SCIENCE-SOURCE0-912468-xx-xSpecialized ApplicationsIncludes Hypersonic Re-entry, Hybrid Runge-Kutta and closed form (subsonic coast).
Includes boomap and R&D source code for bleeding edge programmers.
License includes requirement that users adding value provide a copy of their work.
For use with anything short of orbital insertion.
Supports multi-stage, multi-motor, custom motor.
Download of BASIC source.
ONLY $180.00
USR10-912468-23-8
0-912468-24-6
USR Motor Data Files Disc - PC/MACAirframe and motor files compatible with other software. Download.$10.00
BASIC source code and platform specific shareware runtime module. PC, Mac, Linux, other.
We recommend super or sorb and science-source. Single user multi device license.
Semi-open source, please provide code and language changes for propagation to other users.
Comparison of drag models.
Reference DATCOM (CRP alt/orbit V1984-2009),
RASAERO V1.01, RockSim V8.2.3f4 (2009).
Drag Model comparison>

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