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특허 상세정보

Missile with mid-flight oxidizer charging

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01    F42B-012/52   
출원번호 US-0666965 (2012-11-02)
등록번호 US-9109864 (2015-08-18)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 13

New missile systems are provided, implementing reduced pre-deployment weight, higher impact and greater deployment flexibility, among other advantages. In some embodiments, mid-flight oxygen filtration from atmospheric air, followed by concentration, compression and/or storage in ideal oxidizer deployment locations, leads to enriched, greatly increased oxidizer load and/or far greater missile weight just prior to impact. Among additional benefits, missiles implementing the system may be far less volatile, and therefore safer, prior to deployment and the ...


1. A system for loading a missile after launch, comprising a storage unit volume and a filtering and compressing device configured to load, concentrate and compress gas or other material from the atmosphere surrounding the missile in flight into said storage unit volume, wherein said storage unit volume is configured to store at least some of said gas or other material for deployment at a target. 2. The system for loading a missile after launch of claim 1, wherein said filtering and compressing device is configured to filter out, remove, and concentrate ...

이 특허에 인용된 특허 (13)

  1. Porte, Alain; Chancerelle, Emeric; Alvarez, Franck; Prat, Damien. Air intake arrangement for an aircraft. USP2013038398016.
  2. Grantz Arthur C. (Redondo Beach CA) Bowcutt Kevin G. (Irvine CA) Cervisi Richard T. (Irvine CA). Airbreathing propulsion assisted gun-launched projectiles. USP1996055513571.
  3. McDermott, Brian K.; Greenwood, Kevin R.; Streeter, James D.. Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell. USP2012118312813.
  4. Botwin Leo (Westport CT) Simpson John A. (Southport CT). Gun-launched variable thrust ramjet projectile. USP1984014428293.
  5. Sullivan John D. (Edgewood MD) Kingery Charles N. (Aberdeen MD). High explosive disseminator for a high explosive air bomb. USP1994045303653.
  6. Dyer, Richard S.; Kaemming, Thomas A.; Horne, III, Samuel E.. Multi-path inlet for aircraft engine. USP2012078210474.
  7. Dyer, Richard S; Kaemming, Thomas A; Horne, III, Samuel E. Multi-path inlet for aircraft engine. USP2010057721989.
  8. Cesaroni, Anthony Joseph; Dennett, Michael J.; Kline, Korey R.; Mahaffy, Kevin E.; Smith, Kevin W.. Oxidizer package for propellant system for rockets. USP2003116647888.
  9. Tyll,Jason S.; Bakos,Robert J.; Girlea,Florin; Woelfel,Ralph; Modroukas,Dean; Endos,John I.. Projectile structure. USP2006057051659.
  10. Boyd Robert R.. Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section. USP2000056058846.
  11. Kesting ; Lawrence W.. Solid propellant air turbo rocket. USP1978064096803.
  12. Syberg Jan (Kent WA). Supersonic inlet having variable area sideplate openings. USP1983024372505.
  13. Karanian Arthur J. (Wethersfield CT). Variable-throat chin inlet high Mach number missile application. USP1992125167249.