Study on the heat transfer characteristics of regenerative cooling for LOX/LCH4 variable thrust rocket engine

Author:

Song Jie,Liang Tao,Li Qinglian,Cheng Peng,Zhang Dongdong,Cui Peng,Sun Jun

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Engineering (miscellaneous)

Reference49 articles.

1. Design and test of 15:1 GO2/kerosene variable-thrust rocket engine;Jin;J. Propuls. Technol.,2018

2. System scheme design for LOX/LCH4 variable thrust liquid rocket engines using motor pump;Cui;Acta Astronaut.,2020

3. Flame characteristics of a high-pressure LOX/H2 rocket combustor with large optical access;Martin;Case Studies Thermal Eng.,2021

4. NASA's Space Launch System: Enabling a New Generation of Lunar Exploration;Creech,2019

5. Overview of the chang'e-4 mission: opening the frontier of scientific exploration of the lunar far side;Li;Space Sci. Rev.,2021

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