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Volumn 12, Issue 1, 1996, Pages 41-47

Influence of rocket design parameters on engine nozzle efficiencies

Author keywords

[No Author keywords available]

Indexed keywords

CALCULATIONS; COOLING; EFFECTS; EFFICIENCY; FRICTION; GEOMETRY; KINETIC THEORY; ROCKET ENGINES; SPACE SHUTTLES;

EID: 0029679249     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.23988     Document Type: Article
Times cited : (8)

References (15)
  • 5
    • 0000490999 scopus 로고
    • Exhaust Nozzle Contour for Optimum Thrust
    • June
    • Rao, G. V. R., "Exhaust Nozzle Contour for Optimum Thrust," Jet Propulsion, June 1958.
    • (1958) Jet Propulsion
    • Rao, G.V.R.1
  • 15
    • 85033844701 scopus 로고
    • AIAA Paper 89-2409, July
    • Stohler, S. L., "SSME Update," AIAA Paper 89-2409, July 1989.
    • (1989) SSME Update
    • Stohler, S.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.