Combustion of HMX-CMDB Propellants (II)
β Scribed by Y. Yano; N. Kubota
- Publisher
- John Wiley and Sons
- Year
- 1986
- Tongue
- English
- Weight
- 428 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0721-3115
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
## Abstract Thermal decomposition of BAMO [bis(azidomethyl)oxetane/tetrahydrofuran copolymer]/HMX composite propellants was studied by isothermal TGA (thermogravimetric analysis) and DSC (differential scanning calorimetry) in helium atmosphere, which was showing overall two steps firstβorder kineti
## Abstract The object of this paper is to obtain expressions for the burning rate pressure exponent and the temperature sensitivity of APβbased and HMXβbased CMDB propellants in terms of the respective physical constants on the basis of a recently developed model of combustion for CMDB propellants