摘要
本文简要地叙述了美国研究轨道器与外挂贮油箱,轨道器与载机分离问题的概况。对垂直起飞两级入轨的并联两机的分离问题,提出了研究模型并作了具体分析,着重提出了实现两机安全分离需要解决的技术难点。 二级航天飞机的两机分离问题,是未来航天高技术领域的关键技术之一,本文阐述了解决两体并联分离问题我国现有的技术水平,并提出了解决该问题的技术方案。
The separation research of the Orbiter/External Tank or Orbiter/Carrier in the United States is described in this paper. The analytical model of separation is presented for the parallel Space Shuttle system with the perpendicular launch. Meanwhile, the important problems of the secure separation are presented. The separation of the parallel Space shuttle system is a key technique in the future space technical fields. Our capability of resolving separation is discribed and the method of resolving separation is provided in this paper.
出处
《空气动力学学报》
CSCD
北大核心
1990年第2期174-180,共7页
Acta Aerodynamica Sinica
关键词
航天飞机
载机分离
分离动力学
space shuttle, carrier separation, separation dynamics.
