Ignition time | s | ||
---|---|---|---|
Liftoff time | s | ||
Rod time | s | ||
Rod velocity | m/s | ||
Burnout time | s | ||
Burnout altitude | m | ||
Burnout velocity | m/s | ||
Total impulse | N·s | ||
Specific impulse | s | ||
Exhaust velocity | m/s | ||
Maximum G-load | G | ||
Apogee1 time | s | ||
Apogee altitude | m | ||
Deploy time | s | ||
Deploy altitude | m | ||
Deploy velocity | m/s | ||
Landing time | s | ||
Landing velocity | m/s | ||
1Apogee = maximum altitude
|
This is a very simple model rocket simulation program. It takes published thrust curve data and interpolates that linearly.
Features:
Future improvements I'm considering:
Let me know what you think!