Research Article
A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles
Table 5
Dispersions used in Monte Carlo simulations.
| | Parameter | Mean | Value () | Unit |
| | Specific impulse | 0 | 3 | s | | Mass flow ratio | 0 | 5 | % | | Drag coefficient | 0 | 20 | % | | Lift coefficient | 0 | 20 | % | | Atmospheric density | 0 | 20 | % |
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