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Volumn , Issue , 2001, Pages

Conceptual design of a 'SHARP' - CTV

Author keywords

[No Author keywords available]

Indexed keywords

CONCEPTUAL DESIGN; NASA; REENTRY;

EID: 85087193028     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2887     Document Type: Conference Paper
Times cited : (27)

References (30)
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  • 14
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    • Laminar Heat Transfer Over Blunt Nosed Bodies at Hypersonic Flight Speeds
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  • 15
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    • Minimum Heating Entry Trajectories for Reuseable Launch Vehicles
    • R. Windhorst, M. Ardema, and J. Bowles. "Minimum Heating Entry Trajectories for Reuseable Launch Vehicles". AIAA Journal of Spacecraft and Rockets, 35(5):672-682, 1998.
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    • Windhorst, R.1    Ardema, M.2    Bowles, J.3
  • 16
    • 0027659059 scopus 로고
    • 21st Century Space Transportation System Design Approach: HL-20 Personnel Launch System
    • September-October
    • Howard W. Stone and William M. Piland. "21st Century Space Transportation System Design Approach: HL-20 Personnel Launch System". AIAA Journal of SpaceCraft and Rockets, 30(5):521-528, September-October 1993.
    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 521-528
    • Stone, H.W.1    Piland, W.M.2
  • 17
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    • Aerodynamic Characteristics of the HL-20
    • September-October
    • George M. Ware and Christopher I. Cruz. "Aerodynamic Characteristics of the HL-20". AIAA Journal of SpaceCraft and Rockets, 30(5):529-536, September-October 1993.
    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 529-536
    • Ware, G.M.1    Cruz, C.I.2
  • 18
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    • Six-Degree-of-Freedom Guidance and Control-Entry Analysis of the HL-20
    • September-October
    • Richard W. Powell. "Six-Degree-of-Freedom Guidance and Control-Entry Analysis of the HL-20". AIAA Journal of SpaceCraft and Rockets, 30(5):537-542, September-October 1993.
    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 537-542
    • Powell, R.W.1
  • 19
    • 0027663833 scopus 로고
    • Effect of Lift-to-Drag Ration in Pilot Rating of the HL-20 Landing Task
    • September-October
    • Bruce E. Jackson, Robert A. Rivers, and Melvin L. Bailey. "Effect of Lift-to-Drag Ration in Pilot Rating of the HL-20 Landing Task". AIAA Journal of SpaceCraft and Rockets, 30(5):543-548, September-October 1993.
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    • Jackson, B.E.1    Rivers, R.A.2    Bailey, M.L.3
  • 20
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    • Aerodynamic Heating Environment Definition/Thermal Protection System Selection for the HL-20
    • September-October
    • K. E. Wurster and H. W. Stone. "Aerodynamic Heating Environment Definition/Thermal Protection System Selection for the HL-20". AIAA Journal of SpaceCraft and Rockets, 30(5):549-557, September-October 1993.
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    • Wurster, K.E.1    Stone, H.W.2
  • 21
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    • HL-20 Computational Fluid Dynamic Analysis
    • September-October
    • James K. Weilmuenster and Francis A. Greene. "HL-20 Computational Fluid Dynamic Analysis". AIAA Journal of SpaceCraft and Rockets, 30(5): 558-566, September-October 1993.
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  • 22
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    • Preliminary Structural Evaluation and Design of the HL-20
    • September-October
    • Lance B. Bush, James C. Robinson, and Deborah M. Wahls. "Preliminary Structural Evaluation and Design of the HL-20". AIAA Journal of SpaceCraft and Rockets, 30(5):567-572, September-October 1993.
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    • Bush, L.B.1    Robinson, J.C.2    Wahls, D.M.3
  • 23
    • 0027658608 scopus 로고
    • HL-20 Concept: Design Rational and Approach
    • September-October
    • Carl F. Ehrlich Jr. "HL-20 Concept: Design Rational and Approach". AIAA Journal of SpaceCraft and Rockets, 30(5):573-581, September-October 1993.
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  • 24
    • 0027663294 scopus 로고
    • Design for Effective Development and Prototyping of the HL- 20
    • September-October
    • David M. Urie, Paul A. Floreck, John A. McMorris, and John D. Elvin. "Design for Effective Development and Prototyping of the HL- 20". AIAA Journal of SpaceCraft and Rockets, 30(5):582-589, September-October 1993.
    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 582-589
    • Urie, D.M.1    Floreck, P.A.2    McMorris, J.A.3    Elvin, J.D.4
  • 26
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    • HL- 20 Operations and Support Requirements for the Personnel Launch System Mission
    • September-October
    • W. Douglas Morris and Nancy H. White. "HL- 20 Operations and Support Requirements for the Personnel Launch System Mission". AIAA Journal of SpaceCraft and Rockets, 30(5):597-605, September-October 1993.
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    • Morris, W.D.1    White, N.H.2
  • 29
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    • Evaluation of the National Launch System as a Booster for the HL-20
    • September-October
    • James B. Duffy, Jack W. Lehner, and Bill Pannell. "Evaluation of the National Launch System as a Booster for the HL-20". AIAA Journal of SpaceCraft and Rockets, 30(5):622-627, September-October 1993.
    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 622-627
    • Duffy, J.B.1    Lehner, J.W.2    Pannell, B.3
  • 30
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    • Ascent Abort Capability for the HL-20
    • September-October
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    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 628-633
    • Naftel, J.C.1    Talay, T.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.