Prediction of ignition transients in solid rocket motors employing canted pyrogen igniters

Journal of Propulsion and Power

Volumn 6, Issue 3, 1990, Pages 344-345

  Lal, C Jasper ^a,b   Santha, V ^a,b   Padmanabhan, M S ^a,b  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

^b Heat Transfer and Combustion Research Division ^*  (India)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85002917812     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.25439     Document Type: Article

References (5)

1. Peretz, A, “The starting Transient of Solid Propellant Rocket Motors with High Internal Gas Velocities,” Aerospace and Mechanical Sciences Report No. 1100, Princeton University, Princeton, NJ, April 1973.
2. Caveny, L. H. and Kuo, K. K, “Ignition Transients of Large Segmented Rocket Boosters,” NASA CR-150162, April 1976.
3. Caveny, L. H, “Extensions to Analysis of Ignition Transients of Segmented Rocket Motors,” NASA CR-150632, Jan. 1978.
4. Love, E. S, “Experimental arid Theoretical Studies of Axisymme-tric Free Jets,” NASA TR-R-6, 1959.
5. Martin, H, “Heat and Mass Transfer Between Impinging Gas, Jets and Solid Surfaces,” Advances in Heat Transfer, Vol. 13, 1977.