Research Article
A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles
Table 1
Launch vehicle properties.
| | | Stage 1 | Stage 2 |
| | Total mass (kg) | 16500 | 7093 | | Propellant mass (kg) | 15173 | 5826 | | Mass flow rate (kg/s) | 253 | 89.6 | | Burn time (s) | 60 | 65 | | Specific impulse (s) | 260 | 290 | | Thrust force (N) | 645000 | 248500 | | Reference area (m2) | 3 | 3 |
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