## Abstract The reactions of stabilizers with the individual reactive species known to be generated during double base propellant decomposition, viz. NO~2~, HNO~2~ and HNO~3~, have been thoroughly investigated in an attempt to obtain information on the reactions that take place in these propellant
Assessment scheme for the chemical compatibility of materials with cast double base propellants
β Scribed by G. M. Keeton; D. Facer
- Publisher
- John Wiley and Sons
- Year
- 1992
- Tongue
- English
- Weight
- 420 KB
- Volume
- 17
- Category
- Article
- ISSN
- 0721-3115
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β¦ Synopsis
Abstract
The scheme for the compatibility assessment of materials with cast double base propellants as operated at Royal Ordnance Summerfield is described. Central to the scheme is the recognition that evaluation of the compatibility of materials must consider two areas of safety. These are onβsite process safety requirements, and rocket motor service life which includes safe chemicalstability and the long term functioning and reliability of a store. To rationalize testing, a system of compatibility testing to defined categories classified by the application and usage of a material is followed.
π SIMILAR VOLUMES
## Abstract An unsteady heat conduction model is proposed to calculate the temperature distribution of the caseβbonded rocket motors and the time required for the cooling process based on the experimentally determined thermal and mechanical parameters of a cast modified double base propellant (CMDB