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Volumn 4, Issue , 2007, Pages 3550-3558

Design and development of a 100 km nitrous oxide/paraffin hybrid rocket vehicle

Author keywords

[No Author keywords available]

Indexed keywords

ANEROID ALTIMETERS; LIQUID FUELS; NASA; NITROGEN OXIDES; ROCKETS; SPACECRAFT PROPULSION;

EID: 36749056343     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (41)

References (4)
  • 1
    • 0036575076 scopus 로고    scopus 로고
    • Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
    • May-June
    • Karabeyoglu, M. A., Altman, D., and Cantwell, B. J., "Combustion of Liquefying Hybrid Propellants: Part 1, General Theory," Journal of Propulsion and Power, Vol. 18, No. 3, May-June 2002, pp. 610-620.
    • (2002) Journal of Propulsion and Power , vol.18 , Issue.3 , pp. 610-620
    • Karabeyoglu, M.A.1    Altman, D.2    Cantwell, B.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.