| Citation: | ZHAO Chengeng, SUN Zhongyi, SU Yifei, et al. Investigation the control of the basic thermal environment of multistage launch vehicle at high altitude flight[J]. Journal of Aerospace Power, 2024, 39（12）：20220439 doi: 10.13224/j.cnki.jasp.20220439
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The basic thermal environment of one-engine and four-engine multi-stage liquid launch vehicles has been systematically investigated and the feasibility of the nitrogen injection thermal protection method at the rocket base has been verified by numerical simulation. Based on multi-component Navier-Stokes equation,
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