Fluid-Throat-Induced Shock Waves During the Ignition Transient of Solid Rockets-Reference-Cited by-同舟云学术

Fluid-Throat-Induced Shock Waves During the Ignition Transient of Solid Rockets

Published:2006-01 Issue:1 Volume:43 Page:225-228
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Kumar V. R. Sanal,Kim H. D.,Raghunandan B. N.,Sameen A.,Setoguchi T.¹,Raghunathan S.²

Affiliation:

1. Saga University, Saga 840-8502, Japan

2. Queen’s University of Belfast, Belfast, Northern Ireland BT7 1NN, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.16985

Reference18 articles.

1. Thermoviscoelastic Characterization of a Composite Solid Propellant Using Tubular Test

2. 3Sanal Kumar, V. R. "Flame Spread and Starting Transient in Solid Rocket Motors with Nonuniform Port," Ph.D. Dissertation,Dept. of Aerospace Engineering, Indian Inst. of Science Bangalore, India,Oct. 2001.

3. Ignition transient model for large aspect ratio solid rocket motors

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