首页> 外国专利> RECOVERABLE ROCKET STAGE, ROCKET, AND METHOD FOR LAUNCHING A MULTI-STAGE ROCKET AND RETURNING A RECOVERABLE ROCKET STAGE TO EARTH

RECOVERABLE ROCKET STAGE, ROCKET, AND METHOD FOR LAUNCHING A MULTI-STAGE ROCKET AND RETURNING A RECOVERABLE ROCKET STAGE TO EARTH

机译:可恢复火箭级,火箭以及用于发射多级火箭并将可恢复火箭级返回地球的方法

摘要

A recoverable rocket stage (2) for propelling a rocket (100) towards space includes a rocket propellant tank assembly (4) having a generally cylindrical outer shape; at least one engine (6), coupled to the rocket propellant tank assembly (4); and a plurality of drag enhancing elements (8), the plurality of drag enhancing elements (8) forming longitudinal extensions of the generally cylindrical outer shape of the rocket propellant tank assembly (4) in their launch positions and being inclinable with respect to the generally cylindrical outer shape of the rocket propellant tank assembly (4) for return of the recoverable rocket stage (2) to earth.
机译:一种用于将火箭(100)推向太空的可回收火箭级(2),包括具有大致圆柱形外形的火箭推进剂舱组件(4);至少一个发动机(6),与火箭推进剂箱组件(4)连接;以及多个减阻元件(8),所述多个减阻元件(8)在其发射位置上形成火箭推进剂箱组件(4)的大致圆柱形外形的纵向延伸,并且相对于大致倾斜。火箭推进剂储罐组件(4)的圆柱形外形,用于使可回收火箭级(2)返回地面。

著录项

  • 公开/公告号WO2020099488A1

    专利类型

  • 公开/公告日2020-05-22

    原文格式PDF

  • 申请/专利号WO2019EP81179

  • 发明设计人 BAEKBY BJARNOE JONAS;

    申请日2019-11-13

  • 分类号B64G1;B64G1/40;B64G1/22;F42B10/02;B64G1/64;

  • 国家 WO

  • 入库时间 2022-08-21 11:11:12

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