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특허 상세정보

Mass producible launch system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/40    F42B-015/10    F02K-009/28    F02K-009/00   
미국특허분류(USC) 244/172 ; 102/374 ; 102/377 ; 60/250 ; 60/253 ; 60/255 ; 60/257
출원번호 US-0943432 (1997-10-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Holme Roberts & Owen LLP
인용정보 피인용 횟수 : 16  인용 특허 : 16
초록

The disclosed launch systems are formed from mass producible elements that integrate propulsion, pneumatics and structural systems. In one embodiment, a launch system (10) includes multiple stages (12-16) where each stage includes a number of generally wedge-shaped segments (54). Alternating segments (54) form liquid fuel and oxidizer tanks. Each fuel and oxidizer tank pair is associated with a thruster (70). The resulting plurality of thrusters (70) are disposed about a common aerospike thrust structure (30-34). The segments (54) are connected to an int...

대표
청구항

[ What is claimed is:] [1.] A launch system that has an elongate form with a central, longitudinal axis, comprising:at least a first propulsion element disposed within a first angular region on a first side of said longitudinal axis, including at least a first fuel tank for containing fuel in a fluid phase and a first combustion chamber in selective fluid communication with said first fuel tank;at least a second propulsion element disposed within a second angular region on a second side of said longitudinal axis opposite said first side, comprising at le...

이 특허에 인용된 특허 (16)

  1. Keith Edward L. ; Bauer Thomas P.. Economical launch vehicle. USP1998095799902.
  2. Sneddon Kirk (Sayville NY) Brandmaier Harold (Harrington Park NJ). Fluid storage and expulsion system. USP1995115469701.
  3. Bedegrew Ernest R. (Santa Cruz CA) Chan Allan L. (Pleasanton CA) Connors James J. (Santa Clara CA) Damon Donald E. (Danville CA) Epstein Kenneth W. (San Jose CA) Hada Daniel H. (Cupertino CA) Heath R. Launch vehicle system. USP1996065529264.
  4. Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292). Launch vehicle with interstage propellant manifolding. USP1992085141181.
  5. Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292). Launch vehicle with reconfigurable interstage propellant manifolding and solid rocket boosters. USP1992095143328.
  6. Adachi Kazuhide (No. 3393-7 Banchi Sunagawa ; Tachikawa ; Tokyo JA). Liquid fuel multistage rocket. USP1976013934512.
  7. Thole John M. (Redlands CA) Kelly Michael S. (Redlands CA). Modular solid-propellant launch vehicle and related launch facility. USP1993065217188.
  8. Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292). Multistage launch vehicle employing interstage propellant transfer and redundant staging. USP1992075129602.
  9. Daniels Mark H. (Houston TX) Funk Jack (Houston TX) Evans Wyendell B. (Friendswood TX) Varner Christopher C. (Houston TX). Overlapping stage burn for multistage launch vehicles. USP1990104964340.
  10. Cornelius Charles S. (Huntsville AL) Gibson David A. (Fayetteville TN) Cayson Stephen C. (Harvest AL). Pneumatic separation device. USP1993065218165.
  11. Moore Steven E. (Pleasant View UT) Duce F. Lynn (Brigham City UT). Solid fuel launch vehicle destruction system and method. USP1996045507231.
  12. Kesting ; Lawrence W.. Solid propellant air turbo rocket. USP1978064096803.
  13. . Space launch vehicle. USP1989014796839.
  14. Scott David R. (1300-B Manhattan Ave. Manhattan Beach CA 90266). Space transfer vehicle and integrated guidance launch system. USP1993095242135.
  15. Jones Ernest R. (Ormond Beach FL) Foley James P. (Yardley PA) Dockstader ; Jr. Robert K. (Morrisville PA). Spacecraft adapter and dispenser. USP1995055411226.
  16. Marshall, William R.. Three stage rocket vehicle with parallel staging. USP1984054451017.

이 특허를 인용한 특허 피인용횟수: 16

  1. Robertson, James Hamilton. Adapter for connecting rocket stages. USP2003096622971.
  2. Johnson, Randolph T.. Afterburning aerospike rocket nozzle. USP2003106629416.
  3. Janeke Charl E.,ZAX. Asonic aerospike engine. USP2001046213431.
  4. Ford,Donald B.. Asymmetrical low-profile bulkhead. USP2007087252269.
  5. Facciano, Andrew B; Gonzalez, Juan; Moore, Robert T; Alkema, Michael S. Cluster rocket motor boosters. USP2017019534563.
  6. William James Clark ; Robert John Wetherall. Common bulkhead cryogenic propellant tank. USP2002076422514.
  7. Robert B. Spencer ; Thomas D. Megna ; James R. Greenwood ; Daniel J. Laintz. Fly back booster. USP2002096450452.
  8. Taylor, Zachary R.. Integrated tankage for propulsion vehicles and the like. USP2004066745983.
  9. Taylor,Zachary R.. Integrated tankage for propulsion vehicles and the like. USP2006087093337.
  10. Zachary R. Taylor. Integrated tankage for propulsion vehicles and the like. USP2002126499287.
  11. Stein, William Benjamin; Alexeenko, Alina A.; Hrbud, Ivana; Hitt, Darren L.. Method of enhancing microthruster performance. USP2013128613188.
  12. Wood, James Richard. Missile, chemical plasm steering system, and method. USP20181010113844.
  13. Roger E. Lo DE. Modular solid-fuel rocket charges with rigid support casings. USP2002076421999.
  14. Johnson, Michael David; Hall, Baron. Modular spacecraft. USP2010087780119.
  15. Shi, Zhongwei. Propulsion enhancement arrangement for rocket. USP2010107814835.
  16. Balemboy, Christophe; Laine, Robert Andre; Sembely, Xavier. System comprising a spatial mother probe forming a spatial carrier vehicle and a plurality of spatial daughter probes. USP2015079073646.