An Algebraic Model for Structural and Life Analysis of Regeneratively-Cooled Thrust Chambers-Reference-Cited by-同舟云学术

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An Algebraic Model for Structural and Life Analysis of Regeneratively-Cooled Thrust Chambers

Published:2020-03 Issue:2 Volume:36 Page:191-201
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Pizzarelli Marco¹

Affiliation:

1. Italian Space Agency, 00133 Roma, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference27 articles.

1. CookR. T.FrykE. E.NewellJ. F. “SSME Main Combustion Chamber Life Prediction,” NASA CR-168215, May 1983.

2. Experimental fatigue life investigation of cylindrical thrust chambers

3. KazaroffJ. M.JankovskyR. S.PavliA. J. “Hot Fire Test Results of Subscale Tubular Combustion Chambers,” NASA TP-3222, Nov. 1992.

4. Simplified design and life prediction of rocket thrust chambers

5. PavliA. J.KazaroffJ. M.JankovskyR. S. “Hot Fire Fatigue Testing Results for the Compliant Combustion Chamber,” NASA TP-3223, Sept. 1992.

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2. Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement;J PROPUL POWER;2023

3. A simplified one-dimensional transient heat transfer model for rocket thrust chamber;Applied Thermal Engineering;2023-01

4. Life Analysis of Reusable Liquid Rocket Engine Thrust Chamber;Aerospace;2022-12-02

5. Research on thermomechanical fatigue life prediction of regenerative cooling thrust chamber;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2022-08

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