Thermal-structural analysis for reusable thrust chamber using temperature-dependent CuZr alloy model adapted to cryogenic to elevated temperature-Reference-Cited by-同舟云学术

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Thermal-structural analysis for reusable thrust chamber using temperature-dependent CuZr alloy model adapted to cryogenic to elevated temperature

Published:2024-02 Issue: Volume:145 Page:108782
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Qi Yaqun,Jin Ping,Chen Zhiwei,Lv Junjie,Cai Guobiao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference62 articles.

1. Hybrid multi-objective control allocation strategy for reusable launch vehicle in re-entry phase;Zhang;Aerosp. Sci. Technol.,2021

2. Recovery trajectory planning for the reusable launch vehicle;Cheng;Aerosp. Sci. Technol.,2021

3. Optimal staging of reusable launch vehicles for minimum life cycle cost;Jo;Aerosp. Sci. Technol.,2022

4. Opportunistic preventive maintenance scheduling for multi-unit reusable rocket engine system based on the variable maintenance task window method;Jin;Aerosp. Sci. Technol.,2022

5. Thermal state calculation of chamber in small thrust liquid rocket engine for steady state pulsed mode;Vorobyev;Chin. J. Aeronaut.,2019

Cited by 1 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. Investigation of outgassing properties of CuZr alloy for vacuum chamber structural materials;Nuclear Instruments and Methods in Physics Research Section A: Accelerators, Spectrometers, Detectors and Associated Equipment;2024-09

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