Weight Analysis of Two-Stage-To-Orbit Reusable Launch Vehicles
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES
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