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Volumn 43, Issue 5, 2006, Pages 1124-1130

Vented tank resupply experiment: Flight test results

Author keywords

[No Author keywords available]

Indexed keywords

FLUID DYNAMICS; PROPELLANTS; SPACE SHUTTLES; TANKS (CONTAINERS);

EID: 33750512327     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.18145     Document Type: Article
Times cited : (31)

References (13)
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  • 3
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    • Twenty-three years of surface tension propellant management system design, development, manufacture, test, and operation
    • Rollins, J. R., Grove, R. K., and Jaekle, D. E., Jr., "Twenty-Three Years of Surface Tension Propellant Management System Design, Development, Manufacture, Test, And Operation," AIAA Paper 1985-1199, 1985.
    • (1985) AIAA Paper , vol.1985 , Issue.1199
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  • 4
    • 33750504096 scopus 로고
    • Propulsion Hardware, SE-009-47-01, JPL Contract 953261. Martin Marietta Corporation, Feb.
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    • (1974) Viking Orbiter 1975 System Support, Final Report, Part 2
  • 5
    • 84888853664 scopus 로고
    • The monopropellant hydrazine reaction control system for the RCA SATCOM satellite
    • Balzer, D. L., Brill, Y. C., Scott, W. R., and Sing, P. Y., "The Monopropellant Hydrazine Reaction Control System for the RCA SATCOM Satellite," AIAA Paper 76-631, 1976.
    • (1976) AIAA Paper , vol.76 , Issue.631
    • Balzer, D.L.1    Brill, Y.C.2    Scott, W.R.3    Sing, P.Y.4
  • 6
    • 84888830334 scopus 로고
    • Design and operational performance of the INSAT-I propellant tank
    • Rollins, J. R., and Grove, R. K., "Design and Operational Performance of the INSAT-I Propellant Tank," AIAA Paper 83-1273, 1983.
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    • Rollins, J.R.1    Grove, R.K.2
  • 7
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    • Design, development and flight performance of the mars global surveyor propulsion system
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    • (1999) AIAA Paper , vol.1999 , Issue.2176
    • Dominick, S.M.1
  • 8
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    • Development of the cassini spacecraft propulsion subsystem
    • Leeds, M. W., Eberhardt, R. N., and Berry, R. L., "Development of the Cassini Spacecraft Propulsion Subsystem," AIAA Paper 1996-2864, 1996.
    • (1996) AIAA Paper , vol.1996 , Issue.2864
    • Leeds, M.W.1    Eberhardt, R.N.2    Berry, R.L.3
  • 9
    • 1542605003 scopus 로고    scopus 로고
    • A vane type propellant management device
    • Tegart, J. R., "A Vane Type Propellant Management Device," AIAA Paper 1997-3028, 1997.
    • (1997) AIAA Paper , vol.1997 , Issue.3028
    • Tegart, J.R.1
  • 10
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    • Low-g propellant transfer using capillary devices
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    • Dominick, S.M.1    Tegart, J.R.2
  • 11
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    • Low-g vent testing to support on-orbit fluid resupply systems
    • Bicknell, B.A., and Czysz, P.M., "Low-g Vent Testing to Support On-Orbit Fluid Resupply Systems," AIAA Paper 90-2379, 1990.
    • (1990) AIAA Paper , vol.90 , Issue.2379
    • Bicknell, B.A.1    Czysz, P.M.2
  • 12
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    • Orbital test results of a vaned liquid acquisition device
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  • 13
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    • Capillary rewetung of vaned containers: Spacecraft tank rewetting following thrust resettling
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    • Weislogel, M.M.1    Collicott, S.H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.