메뉴 건너뛰기




Volumn 13, Issue 1, 1997, Pages 164-166

Payload to low earth orbit by aerospace plane with scramjet engine

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; AIRCRAFT FUELS; COMPUTER SIMULATION; HYDROGEN; METHANE; ORBITS;

EID: 0030828220     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.7641     Document Type: Article
Times cited : (21)

References (7)
  • 3
    • 0142048180 scopus 로고
    • Experimental Studies on Aerodynamic Characteristics of SSTO Vehicle at Subsonic to Hypersonic Speeds
    • Committee of International Symposium on Space Technology and Science, Sapporo, Japan
    • Nomura, S., Hozumi, K., Kawamoto, I., and Miyamoto, Y., "Experimental Studies on Aerodynamic Characteristics of SSTO Vehicle at Subsonic to Hypersonic Speeds," Proceedings of the 16th International Symposium on Space Technology and Science, Committee of International Symposium on Space Technology and Science, Sapporo, Japan, 1988, pp. 1547-1554.
    • (1988) Proceedings of the 16th International Symposium on Space Technology and Science , pp. 1547-1554
    • Nomura, S.1    Hozumi, K.2    Kawamoto, I.3    Miyamoto, Y.4
  • 6
    • 0028499582 scopus 로고
    • Effect of Film Cooling/Regenerative Cooling on Scramjet Engine Performances
    • Kanda, T., Masuya, G., Ono, F., and Wakamatsu, Y., "Effect of Film Cooling/Regenerative Cooling on Scramjet Engine Performances," Journal of Propulsion and Power, Vol. 10, No. 5, 1994, pp. 618-624.
    • (1994) Journal of Propulsion and Power , vol.10 , Issue.5 , pp. 618-624
    • Kanda, T.1    Masuya, G.2    Ono, F.3    Wakamatsu, Y.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.