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Volumn , Issue , 2000, Pages

Parametrical analysis of near-term air-breathing engine concepts for first stage space plane acceleration missions

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN; NOZZLE DESIGN; NOZZLES; PROPULSION; ROCKETS; SEA LEVEL; SEPARATION; SPACECRAFT; TURBOFAN ENGINES;

EID: 84896446250     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (2)

References (18)
  • 1
    • 84964546150 scopus 로고
    • A User's Primer for Comparative Assessments of All-Rocket and Rocket-Based Combined-Cycle Propulsion Systems for Advanced Earth-to- Orbit Space Transport Applications
    • AIAA 95-2474, San Diego
    • Escher, W. J. D.; Hyde, E. H.; Andersen, D. M.: A User's Primer for Comparative Assessments of All-Rocket and Rocket-Based Combined-Cycle Propulsion Systems for Advanced Earth-to- Orbit Space Transport Applications, AIAA 95-2474, 31st Joint Propulsion Conference, San Diego 1995
    • (1995) 31st Joint Propulsion Conference
    • Escher, W.J.D.1    Hyde, E.H.2    Andersen, D.M.3
  • 4
    • 84964506775 scopus 로고
    • Evaluation of High Speed Turbojet/Turbofan Engine Concepts on the Performance of the DSL STS-Booster Stage
    • San Diego, AIAA 95-2750
    • Sippel, M.; Sodomann, M.; Deidewig, F.: Evaluation of High Speed Turbojet/Turbofan Engine Concepts on the Performance of the DSL STS-Booster Stage, AIAA 95-2750, 31st Joint Propulsion Conference, San Diego 1995
    • (1995) 31st Joint Propulsion Conference
    • Sippel, M.1    Sodomann, M.2    Deidewig, F.3
  • 5
    • 84896483728 scopus 로고    scopus 로고
    • N. N: DSL Referenz-Daten-Buch, DLR TB-318-96/06
    • N. N: DSL Referenz-Daten-Buch, DLR TB-318-96/06, 1996
    • (1996)
  • 6
    • 0001231735 scopus 로고
    • Turbulent Boundary Layer in Compressible Fluids
    • March
    • van Driest, E. R.: Turbulent Boundary Layer in Compressible Fluids, J. Aeronautical Sciences, V.18, No.3, March 1951, p. 145-160
    • (1951) J. Aeronautical Sciences , vol.18 , Issue.3 , pp. 145-160
    • van Driest, E.R.1
  • 9
    • 84964495111 scopus 로고
    • Research and Development of Turbo Jet Combustor on HST Programme in Japan
    • AIAA 95-2451, San Diego
    • Ogata, H.; Enzaki, Y., Kobayashi, M.; Takagi, N.: Research and Development of Turbo Jet Combustor on HST Programme in Japan, AIAA 95-2451, 31st Joint Propulsion Conference, San Diego 1995
    • (1995) 31st Joint Propulsion Conference
    • Ogata, H.1    Enzaki, Y.2    Kobayashi, M.3    Takagi, N.4
  • 10
    • 0003408567 scopus 로고
    • Preliminary Assessment of Exhaust Systems For High Mach (4 to 6) Fighter Aircraft
    • AIAA 89-2356, Monterey
    • Kuchar, A. P.; Wolf, J. P.: Preliminary Assessment of Exhaust Systems For High Mach (4 to 6) Fighter Aircraft, AIAA 89-2356, 25th Joint Propulsion Conference, Monterey 1989
    • (1989) 25th Joint Propulsion Conference
    • Kuchar, A.P.1    Wolf, J.P.2
  • 18
    • 84896486396 scopus 로고
    • Prediction of Off-Design Performances of Turbojet and Turbofan Engines Based on Gasdynamic Relationships
    • Further information concerning the transportation concept is available at
    • Wittenberg, H.: Prediction of Off-Design Performances of Turbojet and Turbofan Engines Based on Gasdynamic Relationships, Delft University of Technology, 1976 Further information concerning the transportation concept is available at: http://www.kp.dir.de/DSL/
    • (1976) Delft University of Technology
    • Wittenberg, H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.