Radiation effects on 1-D ignition transient analysis of SRM
Author:
Affiliation:
1. Tennessee Technological Univ., Cookeville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3055
Reference14 articles.
1. Starting Transient of Solid-Propellant ocket Motors with High Internal Gas Velocities
2. Ignition transient analysis of a solid rocket motor using a one dimensional two fluid model
3. 2D axisymmetric analysis of SRM ignition transient
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