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AIRBORNE SPACE ANTI-MISSILE SYSTEM

机译:机载空间反导弹系统

摘要

An airborne space anti-missile system provides an offensive anti-missile system that provides a supersonic jet flying in space at 10 times the speed of ultra-high speed jet to deliver air-to-surface missiles towards launch site of an attacking missile. The launching missile is targeted prior to launching or during flight. The supersonic jet comprises: a nuclear plasma jet engine operational in thermosphere, and a stamping jet fusion vector engine or anti-material vector engine for flying in lower atmospheres, no vertical tail and rudder, a pointed wing structure; a fuselage having a length of 60 meters and height of 15 meters, a variable swept wing configuration having a 100° range of wing positions, including a forward position where the wing is disposed forwardly, and wingspan is 200 meters from the fuselage, and a full rearward swept position where wingspan is 60 meters from the fuselage; and electromagnetic space for stealth operations.
机译:机载太空反导系统提供了一种进攻性反导系统,该系统可提供超音速喷气机在太空中飞行,其速度是超高速喷气机的10倍,可将空对地导弹运送到攻击导弹的发射场。发射导弹在发射之前或飞行过程中成为目标。该超音速喷气机包括:在热圈中运行的核等离子体喷气发动机,以及在较低大气中飞行,没有垂直尾翼和舵,尖翼结构的冲压喷气融合矢量发动机或反物质矢量发动机;以及机身长60米,高15米,可变后掠机翼配置,机翼位置在100°范围内,包括机翼向前放置的前向位置,机翼跨距机身200米,以及完全向后掠过的位置,翼展距机身60米;以及用于隐形操作的电磁空间。

著录项

  • 公开/公告号US2019359330A1

    专利类型

  • 公开/公告日2019-11-28

    原文格式PDF

  • 申请/专利权人 SUPERSPACE S&T MANUFACTURE CO. LTD;

    申请/专利号US201815990008

  • 发明设计人 LIGANG ZHAO;

    申请日2018-05-25

  • 分类号B64D1/06;B64C30;B64C3/40;

  • 国家 US

  • 入库时间 2022-08-21 11:19:47

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