首页> 外国专利> CARRIER ROCKET SYSTEM WITH CARRIER ROCKET AND STARTING ASSISTANCE UNIT

CARRIER ROCKET SYSTEM WITH CARRIER ROCKET AND STARTING ASSISTANCE UNIT

机译:带有运载火箭和起动辅助装置的运载火箭系统

摘要

A launch vehicle system 1 is disclosed with a launch vehicle 100 and with a starting aid unit 200 which is detachably connected or can be connected to the launch vehicle 100 . The launch vehicle system 1 is set up to take off in a horizontal launch when thrust is generated by at least one engine 114 (FIG. 1) of the launch vehicle 100 by means of the booster unit 200 . The starting aid unit 200 can be detached from the further-flying carrier rocket 100 after it has reached supersonic speed and is set up to fly back to the earth's surface O after its detachment V/5 from the carrier rocket 100 . The starting aid unit 200 preferably offers all the necessary structural supports for a launch vehicle 100, which was designed for vertical launch, to be able to use this or its essential components without structural changes Launcher system 1.
机译:本发明公开了一种运载火箭系统1,其具有运载火箭100和起动辅助装置200,该装置可拆卸地连接或可连接至运载火箭100。当运载火箭100的至少一个发动机114(图1)通过助推器单元200产生推力时,运载火箭系统1被设置为在水平发射中起飞。起动辅助装置200可在达到超音速后从进一步飞行的运载火箭100上分离,并被设置为在从运载火箭100上分离V/5后飞回地球表面。起动辅助装置200优选地为设计用于垂直发射的运载火箭100提供所有必要的结构支撑,以便能够在不改变运载火箭系统1结构的情况下使用该运载火箭或其基本部件。

著录项

  • 公开/公告号EP3981691A1

    专利类型

  • 公开/公告日2022-04-13

    原文格式PDF

  • 申请/专利权人 ARIANEGROUP GMBH;

    申请/专利号EP20210200510

  • 发明设计人 STOCKFLETH HOLGER;

    申请日2021-10-01

  • 分类号B64G1;B64G1/62;B64G1/64;B64G1/14;

  • 国家 EP

  • 入库时间 2022-08-25 00:31:25

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