Storage-life prediction and relationship between maximum elongation and stabilizer depletion for a composite modified double base propellant (CMDB) propellant
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,General Chemical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s11043-023-09634-8.pdf
Reference39 articles.
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3. Bohn, M.A.: Prediction of life times of propellants – improved kinetic description of the stabilizer consumption. Propellants Explos. Pyrotech. 19(5), 266–269 (2010)
4. Bohn, M.A., Volk, F.: Aging behavior of propellants investigated by heat generation, stabilizer consumption, and molar mass degradation. Propellants Explos. Pyrotech. 17(4), 171–178 (1992)
5. Choi, S.S.: Influence of rubber composition on change of crosslink density of rubber vulcanizates with EV cure system by thermal aging. J. Appl. Polym. Sci. 75(11), 1378–1384 (2000)
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