Aerodynamic analysis of drag, lift force derivative and center of pressure at zero angle of attack
Date: 10/23/2005 Time: 9:12:49 PM
Overall drawing
Parts list of NLV P7
| No. | Designation | Weight | Type | CG | Pitch Inertial Moment | Roll Inertial Moment |
| - | - | (kg) | - | (cm) | (kg*m2) | (kg*m2) |
| 1 | CG Dry | 135.3000 | Fixed | 416.8140 | 2350.61981 | 0.0000000 |
| * | Complete Rocket | 135.3000 | Fixed | 416.8140 | 4701.23962 | 0.0000000 |
| * | Rocket ex. Propellant | 135.3000 | Fixed | 416.8140 | 4701.23962 | 0.0000000 |
CG distances from nosecone apex
Pitch inertial moments around nosecone apex
Roll inertial moments around center axis