Aerodynamic Characterization of Linear Aerospike Nozzles in Off-Design Flight Conditions
Author:
Affiliation:
1. Engine System Research and Development Group, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency, Miyagi 981-1525, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35342
Reference26 articles.
1. Multidisciplinary Approach to Linear Aerospike Nozzle Design
2. Advanced Rocket Nozzles
3. GrossK. W. “Performance Analysis of Aerospike Rocket Engines,” NASA Technical Document 19730004121, Aug. 1972.
4. OnofriM. “Plug Nozzles: Summary of Flow Features and Engine Performance,” AIAA Paper 2002-0584, 2002.
5. X-33 attitude control using the XRS-2200 linear aerospike engine
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