Δ |
|||
---|---|---|---|
0.3 | 0.460 | 0.453 | -0.007 |
0.6 | 0.378 | 0.457 | 0.079 |
0.8 | 0.359 | 0.462 | 0.100 |
1.0 | 0.494 | 0.668 | 0.170 |
1.2 | 0.628 | 0.744 | 0.120 |
1.6 | 0.577 | 0.659 | 0.080 |
2.0 | 0.506 | 0.576 | 0.070 |
2.5 | 0.435 | 0.495 | 0.060 |
3.0 | 0.383 | 0.429 | 0.046 |
Parameter | Value [m] |
---|---|
Total rocket length | 2.000 |
First stage length | 0.983 |
Second stage length | 1.017 |
First stage diameter | 0.135 |
Second stage diameter | 0.045 |
Reference diameter | 0.135 |
Pre-flight distance of centre of mass from the rocket’s base | 0.979 |
Nozzle exit diameter | 0.084 |