Mechanism of Influence of High‐Speed Self‐Spin on Ignition Transients for a Solid Rocket Motor: a Numerical Simulation
Author:
Affiliation:
1. School of Aerospace EngineeringBeijing Institute of Technology Beijing 100081 P.R. China
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201900349
Reference41 articles.
1. M. T. Langhenry Acceleration Effects in Solid Propellant Rocket Motors 22nd Joint Propulsion Conference Huntsville Alabama USA June 16–18 1986 AIAA-86-1577.
2. Aluminized composite solid-propellant burning rates in acceleration fields
3. Effects of grain configuration upon the burning rate of a spinning rocket motor.
4. Experimental evaluation of solid propellant rocket motors under acceleration loads
5. Spin acceleration effects on some full-scale rocket motors.
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