首页> 外国专利> Orbital, Supra Orbital, Sub Orbital, Rocket Propelled, Aerial and Lift Supported Booster Carrier for Flight

Orbital, Supra Orbital, Sub Orbital, Rocket Propelled, Aerial and Lift Supported Booster Carrier for Flight

机译:轨道,超轨道,次轨道,火箭推进,空中和升力支持的助力飞行器

摘要

A rocket-powered, air-deployed, lift-assisted booster vehicle (ALBV) (100) is disclosed for efficiently carrying small payloads to orbital, supraorbital or suborbital altitudes and velocities. The ALBV is secured beneath a conventional carrier aircraft (200) and dropped therefrom at launch altitude and velocity, which contributes significant total energy to the ALBV's ascent trajectory. The ALBV has wings (23), which generate aerodynamic lift to assist in vehicle ascent, and tail fins (24), which perform attitude control while the vehicle is in the sensible atmosphere. After drop launch, an innovative "vertical-S" maneuver is performed using aerodynamic control, causing the ALBV (100) to ascend on a near-theoretical optimal trajectory. In the preferred embodiment, the wings (23) and tail fins (24) are jettisoned as the vehicle exits the sensible atmosphere and aerodynamic lift ceases. This invention represents a dramatic improvement over prior art approaches to orbital payload launch, as it approximately doubles the useful payload that can be carried by the booster compared to identical ground-launched vehicles.
机译:公开了一种火箭动力,空中部署,升力辅助的助推车(ALBV)(100),用于将小的有效载荷有效地运送到轨道,轨道上或亚轨道的高度和速度。该ALBV被固定在常规运载飞机(200)下方,并以发射高度和速度从其降落,这为ALBV的上升轨迹贡献了巨大的总能量。 ALBV具有机翼(23)和尾鳍(24),机翼可产生空气动力学升力以辅助车辆上升,而尾鳍(24)则可在车辆处于敏感环境时进行姿态控制。降落发射后,使用空气动力学控制执行创新的“ vertical-S”操纵,使ALBV(100)沿接近理论的最佳轨迹上升。在优选实施例中,当车辆离开感性大气并且空气动力学升力停止时,机翼(23)和尾鳍(24)被抛弃。本发明代表了对轨道有效载荷发射的现有技术方法的显着改进,因为与相同的地面发射车辆相比,该发明使助推器可以携带的有用有效载荷大约翻倍。

著录项

  • 公开/公告号KR900700840A

    专利类型

  • 公开/公告日1990-08-17

    原文格式PDF

  • 申请/专利权人 레슬리 씨. 씨맨;

    申请/专利号KR19890701643

  • 发明设计人 안토니오 루이스 일라이어스;

    申请日1989-08-31

  • 分类号F41B7/00;

  • 国家 KR

  • 入库时间 2022-08-22 06:12:23

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