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Trajectory Optimization Method in Two-stage-to-orbit RBCC-RKT Launch Vehicle
RUAN Jian'gang, HE Guoqiang, LYU Xiang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2014, (5): 1284 -1291 .  DOI: 10.7527/S1000-6893.2013.0389

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341