[특허]Flyback booster with removable rocket propulsion module

[미국특허] Flyback booster with removable rocket propulsion module 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64G-001/14
출원번호	US-0508504 (2000-08-20)
국제출원번호	PCT/US99/03750 (1998-03-17)
국제공개번호	WO99/47418 (1999-09-23)
발명자 / 주소	Aldrin, Buzz Davis, Hubert P.
출원인 / 주소	Starcraft Boosters, Inc.
대리인 / 주소	Dula, Arthur M.
인용정보	피인용 횟수 : 36 인용 특허 : 6

초록 ▼

A flyback booster (200) comprising an aircraft (203) housing a launch vehicle stage as a removable rocket propulsion module (502) and several space launch vehicles using variations of the flyback booster (200) are disclosed. This flyback booster (200) functions as the first stage of a multistage space launch vehicle. The stage used in the flyback booster (200) and the upper stages of the multistage space launch vehicle (213) are selected to optimize the launch cost for a specific payload.

대표청구항 ▼

1. A flyback booster for vertically launching a payload, releasing the payload and landing on a runway comprising: an aircraft having an airframe made primarily of aluminum designed to operate in the flight regime from vertical launch to Mach 6; a separable rocket propulsion module comprising at least one stage of a space launch vehicle, said module being functionally housed within said aircraft; attachment means for releasably attaching the aircraft to said payload; thrust structure means for transmitting thrust produced by the propulsion module to the payload; landing means including air breathing engine means for providing flight propulsion for the aircraft after said payload has been released until the aircraft lands on said runway; an intelligent aft section flight control means for assisting to control the flight of the aircraft after said payload has been released until the aircraft lands on said runway; said air breathing engine means comprising: a blow off nose releasably fixed to the front to the aircraft; an air inlet configured for supersonic and subsonic operation disposed behind the blow off nose; a pair of turbofan jet engines, each said jet engine having an air intake and a thrust outlet, said engines being disposed side by side within the front of the aircraft and having their air intakes in fluid communication with said air inlet, the centerline of said engines being fixed within the body of the aircraft off the centerline of the aircraft by up to 15 degrees; said jet engine outlets further being in fluid communication with the exterior of the aircraft; and a pair of blow off aerodynamic covers releasably fixed on each side of the aircraft over each of said jet outlets.

이 특허에 인용된 특허 (6) 인용/피인용 타임라인 분석

Martin James A. (Gloucester VA), Integrated launch and emergency vehicle system.
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Thole John M. (Redlands CA) Kelly Michael S. (Redlands CA), Modular solid-propellant launch vehicle and related launch facility.
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Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292), Multistage launch vehicle employing interstage propellant transfer and redundant staging.
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Clapp Mitchell B. ; Zubrin Robert M., Reusable rocket-propelled high altitude airplane and method and apparatus for mid-air oxidizer transfer to said airplane.
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MacConochie Ian O. (Yorktown VA), Shuttle orbiter with telescoping main propulsion unit and payload.
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, Space launch vehicle.
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이 특허를 인용한 특허 (36) 인용/피인용 타임라인 분석

Ishii, Hiroki; Kawasaki, Koji; Matsue, Takenori; Andou, Shinji; Baba, Hiroyasu, Aerial vehicle.
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Chavagnac, Christophe; Bertrand, Jerome; Laporte-Weywada, Hugues; Poulain, Olivier; Matharan, Philippe; Laine, Robert, Aerodynamic and spatial composite flight aircraft, and related piloting method.
상세보기
Chavagnac, Christophe; Bertrand, Jérôme; Laporte-Weywada, Hugues; Poulain, Olivier; Matharan, Philippe; Laine, Robert, Aerodynamic and spatial composite flight aircraft, and related piloting method.
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Speer,Thomas E.; Jones,Richard D., Air vehicle assembly and an associated control system and method.
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Morgan, Robert W; Normoyle, James P; Wuest, Kurt J; Drake, David, Air vehicle with control surfaces and vectored thrust.
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London, Adam P.; Hundley, Lucas A.; Droppers, Lloyd J., Airborne rocket launch system.
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Saint-Jalmes, Bruno; Zaneboni, Jason; Belleville, Mathieu, Aircraft fuselage.
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Cazals, Olivier; Koch, Alexander, Aircraft having a reduced acoustic signature.
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Alber, Mark R., Combined launch and mission vehicles.
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Nowlan, Daniel Ralph, Differential throttling control enhancement.
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Smith, Thomas R.; Bowcutt, Kevin G., First and second stage aircraft coupled in tandem.
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Nakagawa, Shingo; Fukui, Atsushi, Hydraulic apparatus for aircraft actuators.
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Burgener, John A.; Clapp, Mitchell Burnside; DeLong, Daniel Lee, In-flight transfer of reactant from a towing or carrying airplane to an attached rocket or rocketplane.
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Luther, David I., In-line staged horizontal takeoff and landing space plane.
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McKinney,Bevin C.; Hudson,Gary C., Integrated abort rocket and orbital propulsion system.
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Morris, Dennis E.; Little, Alfred, Launch abort and orbital maneuver system.
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Aldrin, Buzz, Multi-crew modules for space flight.
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Troy, John R., Payload delivery vehicle and method.
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Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., Platform and system for mass storage and transfer in space.
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Kistler,Walter P; Citron,Robert A; Taylor,Thomas C, Platform and system for mass storage and transfer in space.
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Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., Platform and system for propellant tank storage and transfer in space.
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Wainfan, Barnaby S.; James, Warren W.; Sokol, Daniel H., Process for recovering a spacecraft first stage.
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Coraboeuf, Yohann; Dutheil, Jean-Philippe, Propulsion unit for reusable launch vehicle.
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Brand, Vance D.; Morgan, Walter Ray, Ram booster.
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Hoover, Randall L., Releasable forward section of an underwater vehicle.
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Salkeld, Robert, Reusable global launcher.
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Prampolini, Marco; Gogdet, Olivier, Reusable module for launcher.
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Helou, Jr., Elie, Space shuttle orbiter and return system.
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Helou, Jr., Elie, Space shuttle orbiter and return system.
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Hall,Allison Earl, Space transportation system.
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Alfano, Salvatore, System and method for assessing the risk of conjunction of a rocket body with orbiting and non-orbiting platforms.
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Smith, Norman Louis, System and method for return and landing of launch vehicle booster stage.
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Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., System and method for transportation and storage of cargo in space.
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Preus, Robert W., System for providing dynamic pitch control in a wind turbine.
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Prampolini, Marco; Coraboeuf, Yohann, Ultra-rapid air vehicle and related method for aerial locomotion.
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Bacon,Richard J., Using imbalanced thrust in a multi-engine jet aircraft.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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[미국특허] Flyback booster with removable rocket propulsion module 원문보기