Combustion response of ammonium perchlorate

AIAA Journal

Volumn 40, Issue 4, 2002, Pages 722-730

  Shusser, Michael ^a   Culick, Fred E C ^b   Cohen, Norman S ^c  

^a California Institute of Technology   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AMMONIUM COMPOUNDS; BOUNDARY CONDITIONS; COMBUSTION; MATHEMATICAL MODELS; PERTURBATION TECHNIQUES;

MONOPROPELLANT AMMONIUM PERCHLORATE;

PROPELLANTS;

EID: 0036530994     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1704     Document Type: Article

References (15)

1. Improved model for the combustion of AP composite propellants
2. Combustion response to compositional fluctuations
3. Effect of AP particle size on combustion response to crossflow
4. Role of turbulence interactions in solid propellant combustion instability
5. Ultra pure ammonium perchlorate T-burner pressure coupled response at 500, 1000, and 1800 psi
6. The steady-state behavior of ammonium perchlorate and HMX
7. Review of calculations for unsteady burning of a solid propellant
8. Model of solid propellant combustion based on multiple flames
9. Surface temperature of deflagrating ammonium perchlorate crystals
10. Numerical solution of solid propellant transient combustion
11. Combustion instabilities: Mating dance of kinetics, combustion and acoustics
12. Stability of longitudinal oscillations with pressure and velocity coupling in a solid propellant rocket
13. Extinction theories and experiments