Influence of Initial Propellant Temperature on Solid Rocket Internal Ballistics
Author:
Affiliation:
1. Department of Aerospace Engineering, Ryerson University, Toronto, Ontario M5B 2K3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35129
Reference16 articles.
1. Powered Flight
2. EXPERIMENTS ON NONLINEAR AXIAL COMBUSTION INSTABILITY IN SOLID PROPELLANT ROCKET MOTORS
3. Effects of Temperature Conditioned Environment on a Propellant's Pressure-Coupled Response
4. EFFECTS OF INITIAL BULK TEMPERATURES ON A PROPELLANT'S PRESSURE-COUPLED RESPONSE
5. Model for Prediction of Negative and Positive Erosive Burning
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