A collaborative analysis tool for integrating hypersonic aerodynamics, thermal protection systems, and RBCC engine performance for single stage to orbit launch vehicles
9th International Space Planes and Hypersonic Systems and Technologies Conference ; 1999 ; Norfolk , VA , U.S.A.
1999-01-01
Conference paper
Electronic Resource
English
Trajectory optimization method in two-stage-to-orbit RBCC-RKT launch vehicle
Online Contents | 2014
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