Nozzle Throat Erosion Characterization Study Using a Solid-Propellant Rocket Motor Simulator-Reference-Cited by-同舟云学术

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Nozzle Throat Erosion Characterization Study Using a Solid-Propellant Rocket Motor Simulator

Published:2007-07-08 Issue: Volume: Page:
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Container-title:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Evans Brian,Kuo Kenneth,Ferrara Peter,Moore Jeffrey,Kutzler Patrick,Boyd Eric

Publisher

American Institute of Aeronautics and Astronautics

Reference2 articles.

1. P. J. Wolt, and J. A. Webber, "Demonstration of a Nozzle BoundaryLayer Cooling System(NBLCS) as a Means to Mitigate Nozzle Erosion," presented atJANNAF 40th Combustion Subcommittee Meeting, Charleston, South Carolina,June13-17,2004.

2. Sutton,G.,Biblarz,O.,RocketPropulsion Elements, 7th Ed.JohnWiley& Sons,NewYork,pp.91, 2001.

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1. Ablation behavior of Al20Si/graphite composite nozzle-throats in a solid rocket motor environment;Ceramics International;2020-06

2. Simple and Accurate Method for Determination of Solid Rocket Motor Nozzle Throat History;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

3. Navier–Stokes Simulation of Graphite Nozzle Erosion at Different Pressure Conditions;AIAA Journal;2015-02

4. Environmental Effects: Ablation of C/C Materials-Surface Dynamics and Effective Reactivity;Ceramic Matrix Composites;2014-10-31

5. Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors;Journal of Propulsion and Power;2014-03

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