Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
2. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
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2. 2Korte, J. J., Salas, A. O., Dunn, H. J., and Alexandrov, N. M. "Multidisciplinary Approach to Linear Aerospike Nozzle Optimization,"AIAAPaper1997-3374,1997.
3. 3Onofri,M."PlugNozzles:SummaryofFlowFeaturesandEnginePerformance,"AIAAPaper2002-0584,2002.
4. 4Hall, C., and Panossian, H. "X-33 Attitude Control Using the XRS-2200 Linear Aerospike Engine," AIAA Paper 1999-2936,1999.
5. Side-Force Amplification on an Aerodynamically Thrust-Vectored Aerospike Nozzle
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