Aeronautics and astronautics – Composite aircraft
Patent
1986-10-14
1989-02-07
Barefoot, Galen
Aeronautics and astronautics
Composite aircraft
244158R, 244160, 244172, 2441374, B64G 114
Patent
active
048026395
ABSTRACT:
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) proceed to staging conditions under air breathing and then rocket power. Rocket engine (22) of aircraft (2) is throttled to produce a thrust differential with rocket engine (66) of vehicle (50). This differential causes vehicle (50) to automatically pivot away from aircraft (2) on struts (30, 32). After pivoting out of cavity (4), vehicle (50) is disengaged from struts (30, 32) and proceeds on its own to orbit. Aircraft (2) makes a conventional landing. Following reentry, vehicle (50) makes an unpowered horizontal landing. Separation is accomplished at a Mach number of about 3.3. In a second embodiment, the main engine of the orbiter (50') is a scramjet (101) instead of a rocket.
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Hardy Jonathan
Hardy Richard
Kornell Thomas J.
Tallquist Kenneth M.
Barefoot Galen
Pauly Joan H.
The Boeing Company
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