Trajectory optimization method in two-stage-to-orbit RBCC-RKT launch vehicle
Hang kong xue bao ; 35 , 5 ; 1284-1291
2014
Aufsatz (Zeitschrift)
Chinesisch
Trajectory Development and Optimization of an RBCC-Based Launch Vehicle (AAS 99-347)
British Library Conference Proceedings | 2000
|Application of a New Economic Analysis Tool to a Two-Stage-to-Orbit RBCC Launch Vehicle Design
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