Starting Transient Flow Phenomena in Inert Simulators of Solid Rocket Motors with Divergent Ports-Reference-Cited by-同舟云学术

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Starting Transient Flow Phenomena in Inert Simulators of Solid Rocket Motors with Divergent Ports

Published:2006-09 Issue:5 Volume:22 Page:1138-1141
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Kumar V. R. Sanal¹,Raghunandan B. N.²,Kim Heuy-Dong³,Sameen A.⁴,Setoguchi T.⁵,Raghunathan S.⁶

Affiliation:

1. Indian Space Research Organization, Trivandrum 695 022, Kerala, India

2. Indian Institute of Science, Bangalore 560 012, India

3. Andong National University, Andong 760-749, Republic of Korea

4. Jawaharlal Nehru Centre for Advanced Scientific Research, Bangalore 560 064, India

5. Saga University, Saga 840-8502, Japan

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

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/10.2514/1.16439

Reference10 articles.

1. Starting Transient of Solid-Propellant ocket Motors with High Internal Gas Velocities

2. Instabilities and pressure oscillations in solid rocket motors

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

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