航天器有效载荷
航天器有效载荷
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随着航天技术的发展,机电系统中不可避免的振动现象对航天器上有效载荷所造成的不良影响变得日益突出。
With the development of space technology , spacecraft payload caused by the adverse effects of the inevitable vibration phenomenon in the electrical and mechanical systems becomes increasingly prominent .
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文中把最大有效载荷的再入轨迹分三种情况作了分析:航天器TPS质量不确定时,通过返回轨迹优化来获得航天器的最大有效载荷,并选择确定相应TPS的质量;
When TPS mas of the space vehicle is determined , the maximum payload is obtained by the design of optimal reentry trafetory ;