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Burning-rate enhancement of a high-energy rocket composite solid propellant based on ferrocene-grafted hydroxyl-terminated polybutadiene binder
D. Saravanakumar, N. Sengottuvelan, V. Narayanan, M. Kandaswamy, T. L. VargheseVolume:
119
Year:
2011
Language:
english
Pages:
8
DOI:
10.1002/app.32859
File:
PDF, 525 KB
english, 2011