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Volumn , Issue , 1999, Pages 1-16

Airbreathing hypersonic technology vision vehicles and development dreams

Author keywords

[No Author keywords available]

Indexed keywords

SPACECRAFT;

EID: 84983213188     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (26)

References (19)
  • 4
    • 84897703424 scopus 로고    scopus 로고
    • Airbreathing, Hypersonic Vision-Operational-Vehicle Design Matrix
    • SAE-1999-01-5515, Presented 1999, San Francisco, CA, Oct. 19-21
    • Hunt, J.L.; Pegg, R.J.; and Petley, D.H.: Airbreathing, Hypersonic Vision-Operational-Vehicle Design Matrix. SAE-1999-01-5515, Presented 1999 World Aviation Congress and Exposition, San Francisco, CA, Oct. 19-21,1999.
    • (1999) World Aviation Congress and Exposition
    • Hunt, J.L.1    Pegg, R.J.2    Petley, D.H.3
  • 6
    • 0005419514 scopus 로고    scopus 로고
    • Appendix A. A Lexicon for Combined-Cycle Hypersonic Propulsion Systems. Society of Automotive Engineers, Inc., Compiled and Edited by William J. D. Escher
    • "The Synerjet Engine. Airbreathing!Rocket Combined-Cycle Propulsion for Tomorrow's Space Transports," Appendix A. A Lexicon for Combined-Cycle Hypersonic Propulsion Systems. Society of Automotive Engineers, Inc., Compiled and Edited by William J. D. Escher., 1997.
    • (1997) The Synerjet Engine. Airbreathing!Rocket Combined-Cycle Propulsion for Tomorrow's Space Transports
  • 12
    • 0016926901 scopus 로고
    • Thermal-Structural Design/Analysis of an Airframe-Integrated Hydrogen-Cooled Scramjet
    • March
    • Wieting, A.R. and Guy, R.W.: Thermal-Structural Design/Analysis of an Airframe-Integrated Hydrogen-Cooled Scramjet. Journal Aircraft, Vol. 1, No 3, March 1976, pp. 192-197.
    • (1976) Journal Aircraft , vol.1 , Issue.3 , pp. 192-197
    • Wieting, A.R.1    Guy, R.W.2
  • 13
    • 84983189864 scopus 로고    scopus 로고
    • Comparative How Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5
    • Presented. Norfolk, Va. AIAA Paper 96-4571, Nov
    • C. McClinton; A. Roudakov; V. Semenov and V. Kopehenov: Comparative How Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5. Presented 7th International Spaceplanes and Hypersonic Systems and Technology Conference. Norfolk, Va. AIAA Paper 96-4571, Nov. 1996.
    • (1996) 7th International Spaceplanes and Hypersonic Systems and Technology Conference
    • McClinton, C.1    Roudakov, A.2    Semenov, V.3    Kopehenov, V.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.