Calculation study on burning rate characteristics of nitramine propellant
- 6 July 1997
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Model and chemistry of HMX combustionAIAA Journal, 1985
- Combustion of RDX/AP composite propellants at low pressuresJournal of Spacecraft and Rockets, 1984
- Modeling Calculations for HMX Composite PropellantsAIAA Journal, 1982
- Combustion of Nitramine PropellantsJournal of Spacecraft and Rockets, 1975
- A model of composite solid-propellant combustion based on multiple flamesAIAA Journal, 1970