๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Thermal decomposition studies on double-base propellant compositions

โœ Scribed by N. Sadasivan; A. Bhaumik


Publisher
Springer Netherlands
Year
1984
Tongue
English
Weight
495 KB
Volume
29
Category
Article
ISSN
0022-5215

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Thermal Decomposition of RDX Composite P
โœ H. Maruizumi; D. Fukuma; K. Shirota; N. Kubota ๐Ÿ“‚ Article ๐Ÿ“… 1982 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 769 KB

## Abstract The thermal decomposition characteristics of RDX, binders, and RDX composite propellants were studied using thermal analytical techniques. Three kinds of binders were tested to elucidate the role of binder on the burning rate of the propellants. There were no apparent correlations betwe

Thermal Decomposition of AMMO/AP Composi
โœ Yoshio Oyumi; Yoshiaki Mitarai; Hakobu Bazaki ๐Ÿ“‚ Article ๐Ÿ“… 1993 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 433 KB

## 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