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Volumn 11, Issue 6, 1995, Pages 1371-1373

Analysis of ignition and flame spreading in solid rocket motor star slots

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; CALCULATIONS; COMPRESSIBLE FLOW; CORRELATION METHODS; FLAME RESEARCH; HEAT RADIATION; IGNITION SYSTEMS; MATHEMATICAL MODELS; PROPELLANTS;

EID: 0029407958     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.51447     Document Type: Article
Times cited : (17)

References (13)
  • 1
    • 0015724833 scopus 로고
    • Starting Transient of Solid-Propellant Rocket Motors with High Internal Gas Velocities
    • Peretz, A., Kuo, K., Caveny, L., and Summerfield, M., “Starting Transient of Solid-Propellant Rocket Motors with High Internal Gas Velocities,” AIAA Journal, Vol. 11, No. 12, 1973, pp. 1719-1727.
    • (1973) AIAA Journal , vol.11 , Issue.12 , pp. 1719-1727
    • Peretz, A.1    Kuo, K.2    Caveny, L.3    Summerfield, M.4
  • 2
    • 0014781921 scopus 로고
    • Prediction of Ignition Transients in Solid Propellant Rocket Motors
    • Sforzini, R. H., and Fellows, H. L., Jr., “Prediction of Ignition Transients in Solid Propellant Rocket Motors,” Journal of Spacecraft and Rockets, Vol. 7, No. 5, 1970, pp. 626-628.
    • (1970) Journal of Spacecraft and Rockets , vol.7 , Issue.5 , pp. 626-628
    • Sforzini, R.H.1    Fellows, H.L.2
  • 5
    • 12944318790 scopus 로고
    • Ignition Transients of Large Segmented Solid Rocket Boosters
    • April
    • Caveny, L. H., and Kuo, K. K., “Ignition Transients of Large Segmented Solid Rocket Boosters,” NASA CR-150162, April 1976.
    • (1976) NASA CR-150162
    • Caveny, L.H.1    Kuo, K.K.2
  • 6
    • 85002917812 scopus 로고
    • Prediction of Ignition Transients in Solid Rocket Motors Employing Canted Pyrogen Igniters
    • Lal, C. J., Santha, V., and Padmanabhan, M., “Prediction of Ignition Transients in Solid Rocket Motors Employing Canted Pyrogen Igniters,” Journal of Propulsion and Power, Vol. 6, No. 3, 1990, pp. 344-345.
    • (1990) Journal of Propulsion and Power , vol.6 , Issue.3 , pp. 344-345
    • Lal, C.J.1    Santha, V.2    Padmanabhan, M.3
  • 7
    • 69249091274 scopus 로고
    • A Numerical Procedure for the Analysis of the Internal Flow in a Solid Rocket Motor During the Ignition Transient Period
    • June
    • Johnston, W. A., “A Numerical Procedure for the Analysis of the Internal Flow in a Solid Rocket Motor During the Ignition Transient Period,” AIAA Paper 91-1655, June 1991.
    • (1991) AIAA Paper 91-1655
    • Johnston, W.A.1
  • 8
    • 85003375857 scopus 로고
    • Numerical Analysis of Ignition Transients in Solid Rocket Motors
    • June
    • Ciucci, A., Jenkins, R. M., and Foster, W. A., Jr., “Numerical Analysis of Ignition Transients in Solid Rocket Motors,” AIAA Paper 91-2426, June 1991.
    • (1991) AIAA Paper 91-2426
    • Ciucci, A.1    Jenkins, R.M.2    Foster, W.A.3
  • 10
    • 85003386518 scopus 로고
    • Final Rept., NASA Marshall Space Flight Center, NAS2-12037, Huntsville, AL, Aug
    • McAnally, J., and Hair, L., “2-D SRM Nozzle-to-Case Joint Test Data Report,” Final Rept., NASA Marshall Space Flight Center, NAS2-12037, Huntsville, AL, Aug. 1988.
    • (1988) 2-D SRM Nozzle-To-Case Joint Test Data Report
    • McAnally, J.1    Hair, L.2
  • 11
    • 0000334985 scopus 로고
    • The Effect of Viscosity in Hypervelocity Impact Cratering
    • April
    • MacCormack, R. W., “The Effect of Viscosity in Hypervelocity Impact Cratering,” AIAA Paper 69-354, April 1969.
    • (1969) AIAA Paper 69-354
    • Maccormack, R.W.1
  • 12
    • 16344365127 scopus 로고
    • Numerical Solution of Axisymmetric Boattail Fields with Plume Simulators
    • Jan
    • Holst, T. L., “Numerical Solution of Axisymmetric Boattail Fields with Plume Simulators,” AIAA Paper 77-224, Jan. 1977.
    • (1977) AIAA Paper 77-224
    • Holst, T.L.1
  • 13
    • 85003355303 scopus 로고
    • private communication
    • Martin, C. L., private communication, 1991.
    • (1991)
    • Martin, C.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.