Aerodynamic analysis of drag, lift force derivative and center of pressure at zero angle of attack
Date: 10/24/2005 Time: 11:10:38 AM
Overall drawing
Parts list of NLV P6
| No. | Designation | Weight | Type | CG | Pitch Inertial Moment | Roll Inertial Moment |
| - | - | (kg) | - | (in) | (kg*m2) | (kg*m2) |
| 1 | CG Dry | 143.2000 | Fixed | 199.2000 | 3665.97180 | 0.0000000 |
| * | Complete Rocket | 143.2000 | Fixed | 199.2000 | 7331.94359 | 0.0000000 |
| * | Rocket ex. Propellant | 143.2000 | Fixed | 199.2000 | 7331.94359 | 0.0000000 |
CG distances from nosecone apex
Pitch inertial moments around nosecone apex
Roll inertial moments around center axis