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Volumn , Issue , 2001, Pages

Hot-firing of an advanced 40 kN thrust chamber

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894325021     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (8)
  • 1
    • 85088722229 scopus 로고    scopus 로고
    • Thrust Chamber Technology Development for Future Launch Vehicle Liquid Rocket Engines
    • AIAA- 01-4841, Salt Lake City, UT
    • Immich, H., Kretschmer, J., Preclik, D., 'Thrust Chamber Technology Development for Future Launch Vehicle Liquid Rocket Engines', AIAA- 01-4841, 37th Joint Propulsion Conference, Salt Lake City, UT, 2001
    • (2001) 37th Joint Propulsion Conference
    • Immich, H.1    Kretschmer, J.2    Preclik, D.3
  • 2
    • 84963860830 scopus 로고    scopus 로고
    • Design Studies for a 10 ton Class High Performance Expander Cycle Engine
    • AIAA-98-3676, Cleveland, OH
    • Schmidt, G., Popp, M., Fröhlich, Th., 'Design Studies for a 10 ton Class High Performance Expander Cycle Engine', AIAA-98-3676, 34th Joint Propulsion Conference, Cleveland, OH, 1998
    • (1998) 34th Joint Propulsion Conference
    • Schmidt, G.1    Popp, M.2    Fröhlich, T.3
  • 3
    • 85085775234 scopus 로고    scopus 로고
    • Technology Developments For Cryogenic Rocket Engines
    • AIAA-2000-3780, Huntsville, AL
    • Immich, H., Kretschmer, J., Preclik, D., 'Technology Developments for Cryogenic Rocket Engines', AIAA-2000-3780, 36th Joint Propulsion Conference, Huntsville, AL, 2000
    • (2000) 36th Joint Propulsion Conference
    • Immich, H.1    Kretschmer, J.2    Preclik, D.3
  • 4
    • 84930794547 scopus 로고    scopus 로고
    • European Research and Technology Test Bench P8 For High Pressure Liquid Rocket Propellants
    • AIAA 2000-3307, Huntsville, AL
    • Haberzettl, A., 'European Research and Technology Test Bench P8 For High Pressure Liquid Rocket Propellants', AIAA 2000-3307, 36th Joint Propulsion Conference, Huntsville, AL, 2000
    • (2000) 36th Joint Propulsion Conference
    • Haberzettl, A.1
  • 5
    • 2042496977 scopus 로고    scopus 로고
    • Flow Separation and Side-Loads in Rocket Nozzles
    • AIAA 99-2815, Los Angeles, CA
    • Frey, M., Hagemann, G., 'Flow Separation and Side-Loads in Rocket Nozzles', AIAA 99-2815, 35th Joint Propulsion Conference, Los Angeles, CA, 1999.
    • (1999) 35th Joint Propulsion Conference
    • Frey, M.1    Hagemann, G.2
  • 7
    • 84943305086 scopus 로고    scopus 로고
    • Design Support for Advanced Storable Propellant Engines by ROCFLAM Analyses
    • AIAA 99- 2459, Los Angeles, CA
    • Knab, O., Frohlich, A., Wennerberg, D., 'Design Support for Advanced Storable Propellant Engines by ROCFLAM Analyses', AIAA 99- 2459, 35th Joint Propulsion Conference, Los Angeles, CA, 1999
    • (1999) 35th Joint Propulsion Conference
    • Knab, O.1    Frohlich, A.2    Wennerberg, D.3
  • 8
    • 84963830520 scopus 로고    scopus 로고
    • Flow Separation and Side-Load Behavior of the Vulcain Engine
    • AIAA 99-2762, Los Angeles, CA
    • Terhardt, M., Hagemann, G., and Frey, M., "Flow Separation and Side-Load Behavior of the Vulcain Engine", AIAA 99-2762, 35th Joint Propulsion Conference, Los Angeles, CA, 1999.
    • (1999) 35th Joint Propulsion Conference
    • Terhardt, M.1    Hagemann, G.2    Frey, M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.