Research Article
Design Optimization and Parameter Analysis of a Hybrid Rocket Motor-Powered Small LEO Launch Vehicle
Table 8
Flight sequence of different cases of SLV.
| | Phase | | | | | | |
| | 1st motor work (s) | 65.2 | 81.2 | 71.0 | 78.7 | 78.5 | 79.1 | | 1st-stage separation (s) | 8.0 | 8.0 | 8.0 | 8.0 | 8.0 | 8.0 | | 2nd motor work (s) | 145.9 | 182.1 | 127.5 | 137.2 | 127.0 | 135.2 | | 2nd-stage separation (s) | 8.0 | 8.0 | 8.0 | 8.0 | 8.0 | 8.0 | | Glide time (s) | 83.3 | 76.0 | 74.3 | 0 | 26.7 | 11.1 | | 3rd motor work (s) | 168.5 | 134.6 | 188.1 | 314.9 | 261.7 | 290.4 | | Total time (s) | 478.9 | 489.9 | 476.9 | 546.8 | 509.9 | 531.8 |
|
|
