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특허 상세정보

Horizontal-takeoff transatmospheric launch system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/14   
미국특허분류(USC) 244/2 ; 244/158R ; 244/160 ; 244/172
출원번호 US-0919207 (1986-10-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 53  인용 특허 : 4
초록

This invention is directed toward providing a transatmospheric launch system that is essentially totally reusable, provides wide flexibility in choice of orbit, and may be launched quickly on short notice. The system of the invention is a two-stage horizontal takeoff and landing system. An orbiter vehicle (50) is integrated into the underside of an aircraft (2). Aircraft (2) has a cavity (4) opening aftwardly and downwardly to receive vehicle (50). Vehicle (50) and aircraft (2) are releasably connected by struts (30, 32). Aircraft (2) and vehicle (50) pr...

대표
청구항

A method of launching a transatmospheric vehicle, comprising: providing an aircraft of the type having an air breathing engine; providing the aircraft with a rocket engine, and providing the transatmospheric vehicle with a scramjet engine; releasably connecting the aircraft and the transatmospheric vehicle together; operating said air breathing engine to accomplish a horizontal takeoff of the connected aircraft and vehicle; flying the connected aircraft and vehicle, including igniting said rocket engine and then accelerating to a Mach number of about 3.3...

이 특허를 인용한 특허 피인용횟수: 53

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