## Abstract The buring rate of ammonium perchlorate (AP) composite propellants is decreased significantly by the addition of SrCO~3~ without increasing the pressure exponent of burning rate. Results of microthermocouple measurements indicate that the burning surface temperature is increased from 70
โฆ LIBER โฆ
Temperature sensitivity of Burning Rate of Ammonium Perchlorate Propellants
โ Scribed by N. Kubota; S. Miyazaki
- Publisher
- John Wiley and Sons
- Year
- 1987
- Tongue
- English
- Weight
- 393 KB
- Volume
- 12
- Category
- Article
- ISSN
- 0721-3115
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