Aerospike engine technology demonstration for space propulsion
Author:
Affiliation:
1. Rockwell International Corp., Rocketdyne Div., Canoga Park, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1974-1080
Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Study of Conical Aerospike Nozzles with Base-Bleed and Freestream Effects;Journal of Spacecraft and Rockets;2019-07
2. Investigating an annular nozzle on combustion products of hydrocarbon fuels;Thermophysics and Aeromechanics;2013-06
3. Studies on Aerodynamic Behavior and Performance of Aerospike Nozzles;Chinese Journal of Aeronautics;2006-02
4. Asymmetric Base-Bleed Effect on Aerospike Plume-Induced Base-Heating Environment;Journal of Propulsion and Power;2004-05
5. Base-Bleed Effect on X-33 Aerospike Plume Induced Base-Heating Environment During Power-Pack Out;36th AIAA Thermophysics Conference;2003-06-23
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