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Volumn 11, Issue 12, 1973, Pages 1719-1727

Starting transient of solid-propellant ocket motors with high internal gas velocities

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS - WAKES; ROCKETS AND MISSILES - PROPELLANTS;

EID: 0015724833     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.50676     Document Type: Article
Times cited : (88)

References (27)
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  • 2
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    • Flame Spreading and Ignition Transients in Solid Grain Propellants
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  • 3
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    • The Ignition Transient in Solid-Propellant Rocket Motors
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    • Parker, K.H.1    Most, W.J.2    Summerfield, M.3
  • 4
    • 85003246182 scopus 로고
    • Theory of a Homogeneous Model of Rocket Motor Ignition Transients
    • Paper 64-127, Palo Alto, Calif
    • Bradley, H. H., Jr., “Theory of a Homogeneous Model of Rocket Motor Ignition Transients,” AIAA Paper 64-127, Palo Alto, Calif., 1964.
    • (1964) AIAA
    • Bradley, H.H.1
  • 6
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    • The Integrated Design Computer Program and the ACP-1103 Interior Ballistics Computer Program
    • Aerojet-General Corp., Sacramento, Calif
    • Threewit, T. R., Rossini, R. A., and Uecker, R. L., “The Integrated Design Computer Program and the ACP-1103 Interior Ballistics Computer Program,” Rept. STM-180, Dec. 1964, Aerojet-General Corp., Sacramento, Calif.
    • (1964) Rept. STM-180
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  • 9
    • 0014752721 scopus 로고
    • A Review of Contemporary Solid Rocket Motor Performance Prediction Techniques
    • Miller, W. H. and Barrington, D. K., “A Review of Contemporary Solid Rocket Motor Performance Prediction Techniques,” Journal of Spacecraft and Rockets, Vol. 7, No. 3, March 1970, pp. 225-237.
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    • Miller, W.H.1    Barrington, D.K.2
  • 10
    • 85003404511 scopus 로고
    • Theory of Ignition and Ignition Propagation of Solid Propellants in a Flow Environment
    • Paper 64-157, Palo Alto, Calif
    • Brown, R. S., Wirrick, T. K., and Anderson, R., “Theory of Ignition and Ignition Propagation of Solid Propellants in a Flow Environment,” AIAA Paper 64-157, Palo Alto, Calif., 1964.
    • (1964) AIAA
    • Brown, R.S.1    Wirrick, T.K.2    Anderson, R.3
  • 12
    • 85007688903 scopus 로고
    • Heat Transfer Characteristics of Hot-Gas Ignition
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  • 18
    • 0002445638 scopus 로고
    • A Simple Equation for Rapid Estimation of Rocket Nozzle Convective Heat Transfer Coefficients
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    • (1957) Jet Propulsion , vol.27 , Issue.1 , pp. 49-51
    • Bartz, D.R.1
  • 19
    • 84987046569 scopus 로고
    • 3rd ed., McGraw-Hill, New York
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  • 21
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  • 22
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  • 23
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    • Goodman, T.R.1
  • 24
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  • 27
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.