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Burning-rate enhancement of a high-energy rocket composite solid propellant based on ferrocene-grafted hydroxyl-terminated polybutadiene binder

✍ Scribed by D. Saravanakumar; N. Sengottuvelan; V. Narayanan; M. Kandaswamy; T. L. Varghese


Publisher
John Wiley and Sons
Year
2010
Tongue
English
Weight
525 KB
Volume
119
Category
Article
ISSN
0021-8995

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