论文部分内容阅读
本文从工程设计角度出发,叙述地球轨道卫星再入大气层的气动加热问题,给出气功加热工程计算方法,并画出典型计算结果。本文可供卫星再入防热系统方案设计和初步设计使用。
In this paper, the aerodynamic heating problem of reentry of earth orbiting satellites into the atmosphere is described from the perspective of engineering design. The calculation method of Qigong heating engineering is given and the typical calculation results are drawn. This article is for the satellite re-entry thermal system design and preliminary design.