Combustion characteristics of high burn rate azide polymer propellant

Propellants, Explosives, Pyrotechnics

Volumn 21, Issue 2, 1996, Pages 74-78

  Nagayama, Kiyokazu ^a   Oyumi, Yoshio ^a  

^a JAPAN DEFENSE AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0042443867     PISSN: 07213115     EISSN: None     Source Type: Journal    
DOI: 10.1002/prep.19960210205     Document Type: Article

References (5)

1. S. Gordon and B. J. McBride, "Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shock and Chapman-Jouguet Detonations", NASA-SP-273, NTIS-N71-37775 (1971).
2. T. Koreki, et al., "Experimental Study on Oscillatory Combustion in Solid-Propellant Motors", J. Spacecraft Rockets 13, 534 (1976).
3. R. L. Coats and M. D. Horton, "Design Considerations for Combustion Stability", ibid. 6, 296 (1969).
4. J. M. Lenoir and G. Robillard, "A Mathematical Method to Predict the Effects of Erosive Burning in Solid Propellant Rockets", 6th Symposium on Combustion (International), (1957), [Proc.], p. 663.
5. E. D. Price and G. A. Flandro, "Combustion Instability in Solid Propellant Rockets", Final Report to Air Force Office of Scientific Research, AD-A216740 (1989).