Improve the thermal performance of precooler by enhancing the utilization of chemical heat sink: Refined design method and characteristic analysis-Reference-Cited by-同舟云学术

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Improve the thermal performance of precooler by enhancing the utilization of chemical heat sink: Refined design method and characteristic analysis

Published:2024-10 Issue: Volume:254 Page:123853
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Xu Yusen,Wang Yifan,Du Pengcheng,Liu Huoxing,He Kun,Chen Yiming,Yao Lichao

Publisher

Elsevier BV

Reference47 articles.

1. A comparison of propulsion concepts for SSTO reusable launchers;Varvill;J-Br. Interplanet. Soc.,2003

2. Progress in research of thermodynamic cycle of hypersonic precooled engine;Wang;Acta. Aeronaut. Astronaut. Sin.,2023

3. Development study on ATREX engine;Sato;Acta. Astronaut,2000

4. M. Hempsell, Progress on the SKYLON and SABRE, in: Proceedings of the international astronautical congress. 2013;IAC-13.D2.4.6x19609.

5. J. Bartha, H. Webber, SABRE technology development. 67th international astronautical congress, 2016;IAC-16-C4.9.2, 2016.

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