Study of Initial Pressure Rise in Multi Grain Solid Propellant Rocket Motor
Author:
Affiliation:
1. High Energy Material Research Laboratory 411021 Pune
2. Defence Institute of Advanced Technology 411025 Pune
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201900291
Reference17 articles.
1. G. Sutton O. Biblarz Rocket Propulsion Elements John Wiley & Sons Inc.2001 45–75 417–53 520–26.
2. B. Zeller Solid Propellant Grain Design. In: A. Davenas Solid Rocket Propulsion Technology Elsevier 1993 pp. 35–84). Retrieved from http://linkinghub.elsevier.com/retrieve/pii/B9780080409993500072.
3. Anomalous Behavior of a Solid Rocket Motor Nozzle Insert During Static Firing Test
4. Solving an Irregular Burning Problem in a Small Rocket Motor;Gligorijević N.;Sci.-Tech. Rev.,2014
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