Extinguishment of solid propellants by depressurization - Effects ofpropellant parameters
- 20 January 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Low Pressure Burning of Composite Solid PropellantsPublished by American Chemical Society (ACS) ,1969
- A review of calculations for unsteady burning of a solid propellant.AIAA Journal, 1968
- Extinguishment of solid propellants by rapid depressurization.AIAA Journal, 1968
- Role of Aluminum in Suppressing Instability in Solid Propellant Rocket MotorsPublished by Defense Technical Information Center (DTIC) ,1968
- Initial pressure peaks in rocket motors and interruption by venting.Journal of Spacecraft and Rockets, 1968
- Surface reaction effects on the acoustic response of composite solidpropellants.AIAA Journal, 1968
- Depressurization induced extinction of burning solid propellant.AIAA Journal, 1968
- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961
- Burning Mechanism of Ammonium Perchlorate PropellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1960