首页> 外国专利> DEVICE FOR CONTROLLING THE SPEED OF A SPATIAL AIRCRAFT DURING THE TRANSITION OF A SPATIAL FLIGHT PHASE TO AN AERONAUTICAL FLIGHT PHASE AND THE TRANSITION METHOD THEREOF

DEVICE FOR CONTROLLING THE SPEED OF A SPATIAL AIRCRAFT DURING THE TRANSITION OF A SPATIAL FLIGHT PHASE TO AN AERONAUTICAL FLIGHT PHASE AND THE TRANSITION METHOD THEREOF

机译:在将空间飞行阶段转换为航空飞行阶段期间控制空间飞机速度的装置及其转换方法

摘要

Spatial aircraft adapted to an aeronautical flight comprising a body and a wing defining a lower bearing surface as well as attitude control means which comprises one or more flaps arranged under its lower bearing surface and maneuverable between a retracted position and an inclined out position aerodynamic braking during the transition from a phase of spaceflight to an aeronautical flight phase of the aircraft.
机译:适用于航空飞行的空间飞行器,包括限定下部支承表面的机体和机翼,以及姿态控制装置,该姿态控制装置包括一个或多个襟翼,这些襟翼布置在其下部支承表面下方并可在缩回位置和倾斜位置之间进行气动制动从太空飞行阶段过渡到飞机的航空飞行阶段。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号