摘要: The optimization of trajectories for coplaner, aeroassisted orbital transfer(AOT) from a high Earth orbit (HEO) to a low Earth orbit (LEO) is examined. In particular, HEO can be a geosynchronous Earth orbit (GEO). It is assumed th... 展开
作者 | Miele, A. Wang, T. Deaton, A. W. | ||
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原报告号 | N9114366 | 总页数 | 58 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Spacecraft trajectories Trajectory optimization Transfer orbits Aeroassist Aerobraking Atmospheric entry Orbit transfer vehicles Spacecraft guidance Aerodynamic coefficients Aerodynamic heating Coriolis effect Dynamic pressure Earth orbits Ea |