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Thermal Decomposition Kinetics of Kerosene-Based Rocket Propellants. 2. RP-2 with Three Additives †

✍ Scribed by Widegren, Jason A.; Bruno, Thomas J.


Book ID
120465303
Publisher
American Chemical Society
Year
2009
Tongue
English
Weight
885 KB
Volume
23
Category
Article
ISSN
0887-0624

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## 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