Ascent Trajectory Optimisation for a Single-Stage-to-Orbit Vehicle with Hybrid Propulsion
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
ASCENT TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION
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