Rocket combustion chamber life-enhancing design concepts-Reference-Cited by-同舟云学术

Rocket combustion chamber life-enhancing design concepts

Published:1990-07-16 Issue: Volume: Page:
ISSN:
Container-title:26th Joint Propulsion Conference
language:
Short-container-title:

Author:

QUENTMEYER R.¹

Affiliation:

1. NASA, Lewis Research Center; Sverdrup Technology,Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2116

Reference33 articles.

1. Conway, J.B.; Stentz,R.H.;and Berling, J.T.:High Temperature,Low-Cycle Fatigue of Copper-Base Alloys in Argon. Part I: Preliminary Results for 12 Alloys at 1000 "F (538 "C). NASA CR-121259, 1973.

2. (Mar-Test,Inc.,NASA Contract NAS3-16753)

3. zle Materials. (Boeing Aerospace Co.,NASA Contract NAS3-17838) NASA

4. CR-134806, 1975.

5. space Co.,NASA Contract NAS3-17838) NASA CR-134822, 1975.

Cited by 26 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An analytical formula evolved from thermal-structural coupling model for life prediction and structural design of reusable thrust chambers;Applied Thermal Engineering;2024-08

2. Continuum model template to analyze complex parameters for engine cooling;Journal of Mechanical Science and Technology;2024-01

3. Heat Transfer Analysis and Structural Optimization for Spiral Channel Regenerative Cooling Thrust Chamber;International Journal of Aerospace Engineering;2023-06-14

4. Thermal mechanical analysis of novel electron collector for megawatt class gyrotrons;24TH TOPICAL CONFERENCE ON RADIO-FREQUENCY POWER IN PLASMAS;2023

5. Research on copper erosion in hydrogen peroxide/kerosene bipropellant thrust chamber;Acta Astronautica;2021-11