## Abstract Thermal decomposition of AMMO/AP composite propellants was studied by DTA, TGA and DSC in helium atmosphere. The effects of accelerated aging at 347 K for 370 days on decomposition kinetics were also measured. AMMO/AP propellant showed two different decomposition steps, which were mainl
โฆ LIBER โฆ
Thermal decomposition of cured GAP-AP propellants containing catocene
โ Scribed by Shin-Ming Shen; Shao-Wun Wang; Yih-Shun Chiu; Sun-I Chen; Fang-Mo Chang; Chen-Chia Huang
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 690 KB
- Volume
- 216
- Category
- Article
- ISSN
- 0040-6031
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## Abstract A modified manometric vacuum stability test (MVST) apparatus as well as a differential thermal analyzer (DTA) and a thermogravimetric analyzer (TGA) were used to study thermal decomposition of a series of propellants. The solid propellants contained polycaprolactone (PCP) prepolymer or