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Combustion of HMX-CMDB Propellants (II)

✍ 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

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πŸ“œ SIMILAR VOLUMES


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## 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 first‐order kineti

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