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Volumn 24, Issue , 2006, Pages 18215-18227

Visualization of a capsule entry vehicle reaction-control system (RCS) thruster

Author keywords

[No Author keywords available]

Indexed keywords

CAPSULE ENTRY VEHICLE REACTION; FAR FIELDS; JET PLUMES; THRUSTERS;

EID: 34250840063     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (13)

References (21)
  • 1
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    • See, html and, http://www.nasa.gov/pdf/133654main_ESAS_charts.pdf
    • See http://www.nasa.gov/mission_pgaes/exploration/spacecraft/cev. html and http://www.nasa.gov/pdf/133654main_ESAS_charts.pdf.
  • 2
    • 17644389551 scopus 로고    scopus 로고
    • From Mercury to CEV: Space Capsules Reemerge
    • Feb
    • F. Sietzen Jr., "From Mercury to CEV: Space Capsules Reemerge," Aerospace America, p. 26-33, Feb (2005).
    • (2005) Aerospace America , pp. 26-33
    • Sietzen Jr., F.1
  • 4
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    • Molecular velocity imagining of supersonic flows using pulsed planar laser-induced fluorescence of
    • Paul PH, Lee MP, Hanson RK, Molecular velocity imagining of supersonic flows using pulsed planar laser-induced fluorescence of NO, Opt. Lett., Vol. 14, 417-419 (1989).
    • (1989) Opt. Lett , vol.14 , pp. 417-419
    • Paul, P.H.1    Lee, M.P.2    Hanson, R.K.3
  • 5
    • 0027710984 scopus 로고
    • Temporally resolved, two-line fluorescence imaging of NO in a transverse jet in a supersonic cross-flow
    • McMillin BK, Palmer JL and Hanson RK, "Temporally resolved, two-line fluorescence imaging of NO in a transverse jet in a supersonic cross-flow," Appl. Opt., 32, 7532 (1993).
    • (1993) Appl. Opt , vol.32 , pp. 7532
    • McMillin, B.K.1    Palmer, J.L.2    Hanson, R.K.3
  • 9
    • 0029753186 scopus 로고    scopus 로고
    • Comparison of planar fluorescence measurements and computational modeling of a shock layer flow
    • Houwing AFP, Palmer JL, Thurber MC, Wehe SD, Hanson RK, Boyce RR, Comparison of planar fluorescence measurements and computational modeling of a shock layer flow, AIAA Journal, Vol. 34 (3), 470-477 (1996).
    • (1996) AIAA Journal , vol.34 , Issue.3 , pp. 470-477
    • Houwing, A.F.P.1    Palmer, J.L.2    Thurber, M.C.3    Wehe, S.D.4    Hanson, R.K.5    Boyce, R.R.6
  • 12
    • 0141461660 scopus 로고    scopus 로고
    • Fluorescence Imaging of Rotational and Vibrational Temperature in a Shock Tunnel Nozzle Flow
    • Sept. p, 2003
    • P. C. Palma, P. M. Danehy, A. F. P. Houwing, "Fluorescence Imaging of Rotational and Vibrational Temperature in a Shock Tunnel Nozzle Flow," AIAA Journal, Vol. 41, no. 9, Sept. p. 1722-1732 (2003).
    • AIAA Journal , vol.41 , Issue.9 , pp. 1722-1732
    • Palma, P.C.1    Danehy, P.M.2    Houwing, A.F.P.3
  • 16
    • 0037325073 scopus 로고    scopus 로고
    • Flow-tagging velocimetry for hypersonic flows using fluorescence of nitric oxide
    • P. M. Danehy, S. O'Byrne, A.F.P. Houwing, J.S. Fox, D.R. Smith "Flow-tagging velocimetry for hypersonic flows using fluorescence of nitric oxide," AIAA Journal v. 41, n. 2, p. 263-271 (2003).
    • (2003) AIAA Journal , vol.41 , Issue.2 , pp. 263-271
    • Danehy, P.M.1    O'Byrne, S.2    Houwing, A.F.P.3    Fox, J.S.4    Smith, D.R.5
  • 18
    • 84982318849 scopus 로고    scopus 로고
    • J. R. Micol Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities, AIAA Paper 98-0147, 36th AIAA Aerospace Sciences Meeting & Exhibit, January 12-15, Reno, NV (1998).
    • J. R. Micol "Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities," AIAA Paper 98-0147, 36th AIAA Aerospace Sciences Meeting & Exhibit, January 12-15, Reno, NV (1998).
  • 19
    • 0034283085 scopus 로고    scopus 로고
    • The RELIEF flow tagging technique and its application in engine testing facilities and for helium-air mixing studies
    • R B Miles, J Grinstead, R H Kohl and G Diskin "The RELIEF flow tagging technique and its application in engine testing facilities and for helium-air mixing studies," Meas. Sci. Technol. v. 11, p. 1272-1281 (2000).
    • (2000) Meas. Sci. Technol , vol.11 , pp. 1272-1281
    • Miles, R.B.1    Grinstead, J.2    Kohl, R.H.3    Diskin, G.4
  • 20
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    • ViDI: Virtual Diagnostics Interface Volume 1-The Future of Wind Tunnel Testing
    • NASA/CR-2003-212667, December 2003
    • Schwartz, R.J., "ViDI: Virtual Diagnostics Interface Volume 1-The Future of Wind Tunnel Testing" Contractor Report NASA/CR-2003-212667, December 2003
    • Contractor Report
    • Schwartz, R.J.1
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    • http://www.autodesk.com/


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.