Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors-Reference-Cited by-同舟云学术

Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors

Published:2014-03 Issue:2 Volume:30 Page:314-324
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Turchi Alessandro¹,Bianchi Daniele¹,Thakre Piyush²,Nasuti Francesco¹,Yang Vigor³

Affiliation:

1. Dipartimento di Ingegneria Meccanica e Aerospaziale, University of Rome “La Sapienza,” 00184 Rome, Italy

2. CD-adapco, Ltd., Melville, New York 11747

3. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0150

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.B34997

Reference43 articles.

1. KowalT. J. “Thermal Protection System (Heat Shield) Development: Advanced Development Project,” Commercial Human Spaceflight Symposium, NASA Rept. JSC-CN-21831, Houston, TX, Oct. 2010.

2. Vega Solid Rocket Motors Development and Qualification

3. A semiquantitative prediction of the erosion of graphite nozzle inserts

4. Erosion of graphite in solid-propellant combustion gases and effects on heat-transfer

5. A Comprehensive Theoretical Model for Carbon-Carbon Composite Nozzle Recession

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