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J-GLOBAL ID:200902267033669214   Reference number:07A0766414

Design of Sub-Scale Rocket-Ramjet Combined Cycle Engine Model

ロケット-ラムジェット複合サイクルエンジン・サブスケールモデルの設計
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Issue: 06-009E  Page: 18P  Publication year: Feb. 28, 2007 
JST Material Number: G0143B  ISSN: 1349-1113  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: ENGLISH (EN)
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Other heat engines 
Reference (28):
  • http://www.jaxa.jp/about/vision_mission/long_term/index_e.html
  • Siebenhaar, A., “Strutjet Evolves to Meet Air-Breathing Propulsion Challenges for the 21st Century,” 13th International Symposium on Air-Breathing Engines, Paper 97-7135, Sep. 1997.
  • Andreadis, D., Drake, A., Garrett, J. L., Gettinger, C. D., and Hoxie, S. S., “Design Consideration of ISTAR Hydrocarbon Fueled Combustor Operating Air Augmented Rocket, Ramjet and Scramjet Modes,” 11th AIAA/AAAF International Conference on Space Planes and Hypersonic Systems and Technologies Paper, Orleans, France, Sep. 2002.
  • Lee, J., and Krivanek, T., “Design and Fabrication of the ISTAR Direct-Connect Combustor Experiment at the NASA Hypersonic Tunnel Facility,” AIAA Paper, AIAA-2005-0611, Jan.2005.
  • Heiser, W. H., Pratt, D. T., Daley, D. H., and Mehta, U. B., “Hypersonic Airbreathing Propulsion,” AIAA Education Series, AIAA, Washington, DC, 1994, pp. 447-451.
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