The Mechanism of Ignition of Composite Solid Propellants by Hot Gases
- 1 January 1960
- book chapter
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Analysis of a Simplified Model of Solid Propellant Resonant BurningJournal of the Aerospace Sciences, 1959
- Some Properties of a Simplified Model of Solid Propellant BurningJournal of Jet Propulsion, 1958
- Some Effects of Oxidizer Concentration and Particle Size on Resonance Burning of Composite Solid PropellantsJournal of Jet Propulsion, 1958
- Observations on the Irregular Reaction of Solid Propellant ChargesJournal of Jet Propulsion, 1956
- A Mechanism for High-Frequency Oscillation in Ramjet Combustors and AfterburnersJournal of Jet Propulsion, 1956
- A Theoretical and Experimental Study of Shock-Tube FlowsJournal of the Aeronautical Sciences, 1955
- Theory of Ignition Considered as a Thermal ReactionThe Journal of Chemical Physics, 1954
- The A Physical Theory of Burning of Double-Base Rocket Propellants. I.The Journal of Physical Chemistry, 1950
- The The Theory of the Burning of Double-Base Rocket Powders.The Journal of Physical Chemistry, 1950