GENERALIZED VEHICLE PERFORMANCE CLOSURE MODEL FOR TWO-STAGE-TO-ORBIT LAUNCH VEHICLES
42nd:; Meeting, Aerospace sciences ; 2004 ; Reno, NV
2004-01-01
AIAA 2004-1221
AIAA 2004-0001 - AIAA 2004-1388 held with gaps
Conference paper
English
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Two-Stage-To-Orbit Reusable Launch Vehicle Propulsion Performance Study
British Library Conference Proceedings | 2004
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