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Volumn 38, Issue 1, 2001, Pages 36-42

Concept and preliminary flight testing of a fully reusable rocket vehicle

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTICS; FLIGHT DYNAMICS; LANDING; ROCKET ENGINES; SOUNDING ROCKETS;

EID: 0035082390     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3652     Document Type: Article
Times cited : (50)

References (8)
  • 3
    • 0005758357 scopus 로고    scopus 로고
    • A concept of reusable sounding rocket with enhanced maneuverability and operability
    • International Symposium on Space Technology and Science, Tokyo
    • Inatani, Y., Naruo, Y., and Yamada, T., "A Concept of Reusable Sounding Rocket with Enhanced Maneuverability and Operability," Proceedings of the 20th International Symposium on Space Technology and Science, International Symposium on Space Technology and Science, Tokyo, 1996, pp. 1165-1170.
    • (1996) Proceedings of the 20th International Symposium on Space Technology and Science , pp. 1165-1170
    • Inatani, Y.1    Naruo, Y.2    Yamada, T.3
  • 5
    • 0005758358 scopus 로고
    • Society of Automotive Engineers, SAE Technical Series 892269, Sept.
    • Schmidgall, R. A., "Space Shuttle Ascent Abort," Society of Automotive Engineers, SAE Technical Series 892269, Sept. 1989.
    • (1989) Space Shuttle Ascent Abort
    • Schmidgall, R.A.1
  • 6
    • 0005692263 scopus 로고    scopus 로고
    • Throttling dynamic response of LH2 rocket engine for vertical landing rocket vehicle
    • American Astronautical Society, San Diego, CA
    • Naruo, Y., Inatani, Y., Morita, Y., Nakai, S., and Mori, H., "Throttling Dynamic Response of LH2 Rocket Engine for Vertical Landing Rocket Vehicle," Advances in the Astronautical Sciences, Vol. 96, American Astronautical Society, San Diego, CA, 1997, pp. 229-240.
    • (1997) Advances in the Astronautical Sciences , vol.96 , pp. 229-240
    • Naruo, Y.1    Inatani, Y.2    Morita, Y.3    Nakai, S.4    Mori, H.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.