Research on Matching Discipline between Primary Rocket and RBCC Engine
Author:
Affiliation:
1. China Academy of Launch Vehicle Technology
2. Northwestern Polytechnical University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2296
Reference12 articles.
1. S. Chiesa, M. Grassi, G. Russo. A small-Scale Low-Cost Technology Demonstrator of aReusable LaunchVehicle[R].AIAAPaper2005-3346.
2. Joseph M. Hank, Milton E. Franke, Dean R. Eklund. TSTO Reusable Launch Vehicles UsingAirbreathing Propulsion[R].AIAAPaper 2006-4962.
3. Alicia R. Hartong, Brendan D. Rooney. Near-Term RLV Options[R]. AIAA Paper 2004-5947.
4. Richard W. Foster, William J. D. Escher et al. Studies of an ExtensivelyAxisymmetric Rocket Based Combined Cycle (RBCC) Engine Powered Single-Stage-to-Orbit (SSTO) Vehicle[R].AIAA-89-2294,1989.
5. Andrews E. H. Scramjet Development and Testing in the United States[R], AIAA-2001-1927.
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