PML Matrix Simulation Results
First Stage Mass = 1425 grams
CG Position = 821 mm
Motor Mount = 38 mm
| Deploy | Engine | Delay | Max Altitude | Max Velocity | Max Accel. | Optimal Delay | Comments |
| OK | H153 | 10 | 1971 | 128 | 101 | 9.2 | Pro38 Classic |
| OK | I205 | 11 | 2970 | 181 | 121 | 10.9 | Pro38 Classic |
| OK | I285 | 12 | 3781 | 227 | 173 | 11.9 | Pro38 Classic |
| OK | J285 | 12 | 4562 | 264 | 174 | 12.4 | Pro38 Classic |
| OK | H143SS | 10 | 1849 | 121 | 85 | 9 | Pro38 SS |
| OK | I212SS | 10 | 2721 | 170 | 127 | 10.4 | Pro38 SS |
| OK | I287SS | 12 | 3510 | 216 | 164 | 11.7 | Pro38 SS |
| OK | I350SS | 13 | 4120 | 248 | 173 | 12.6 | Pro38 SS |
Key:
Deploy: deployment status (early, late, at apogee or crash)
Engine: motor type used
Delay: delay used for that flight
Max Altitude: in feet
Max Velocity: in ms^-1
Max Accel.: in ms^-2
Optimal Delay: best delay to use in seconds
This page has been automatically generated from the Rocksim .rkt file.
Copyright 1995-2005 A.S.Moore. All Rights Reserved.
