摘要
再入飞行器的试验运载火箭弹道设计一般考虑飞行器的再入模拟量及落地要求、火箭飞行试验的航区要求、火箭的技术状态等3个主要因素,为此开展弹道实现模式及特征速度分析,得出弹道设计中"第2次冲量"的施加技术方案。
Several factors are considered into the experimental launch trajectory design for re-entry vehicle,including re-entry parameters and impact requirements,flight corridor and technical state of launch vehicle.The trajectory realization mode and characteristic velocity are analyzed to obtain the technical scheme of the second impulse in trajectory design.
出处
《航天控制》
CSCD
北大核心
2015年第5期17-21,共5页
Aerospace Control
关键词
试验
运载火箭
再入
弹道设计
Experiment
Launch-vehicle
Re-entry
Trajectory design
