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Projectile diverter

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00   
미국특허분류(USC) 244/00322; 244/00321; 102/501
출원번호 US-0502119 (2000-02-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Robert Moll
인용정보 피인용 횟수 : 14  인용 특허 : 2
초록
▼

The present invention provides a fast, low-cost, small diverter capable of generating a relatively high impulse (1-5 N-sec) over a short time period. The diverter is adapted for installation in a projectile for steering the projectile in flight by ejecting an end cap in response to control signals from a guidance system. In one embodiment, multiple diverters are arranged in one or more bands about a flying projectile such as a rocket. Each diverter includes a header assembly providing a mounting surface and support for a plurality of electrical leads, a ...

대표
청구항
▼

1. A projectile diverter, comprising:a header assembly providing a mounting surface and support for a plurality of electrical leads; a reactive semiconductor bridge mounted on the mounting surface of the header assembly and providing an electrical path for the electrical leads at a certain voltage across the bridge; a diverter body supporting the header assembly and containing a prime, wherein the reactive semiconductor bridge ignites the prime; and an end cap attached to the diverter body and containing a propellant, wherein the rapid burning of the pro...

이 특허에 인용된 특허 (2)

  1. Bains William R. (Lake Elsinore CA). Pneumatically actuated ram air steering system for a guided missile. USP1987084685639.
  2. Morenus Richard C. (Long Beach CA) Frazer Alson C. (Santa Ana CA). Ram air combustion steering system for a guided missile. USP1986034573648.

이 특허를 인용한 특허 피인용횟수: 14

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  3. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  4. Heitmann,Thomas; Schwenzer,Michael. Lateral thrust control. USP2006107118065.
  5. Gnemmi, Patrick; Rey, Christian. Low voltage device for the generation of plasma discharge to operate a supersonic or hypersonic apparatus. USP2010017645969.
  6. Low, Richard; Deeds, Michael; Jean, Daniel L.; Hovland, Christopher. MEMS control surface for projectile steering. USP2009127628352.
  7. Boucher,Craig J.; Marshall,Paul N.; Novotney,David B.. Ordinance firing system for land vehicle. USP2007107278658.
  8. Boucher, Craig J.; Marshall, Paul N.; Novotney, David B.. Ordnance firing system. USP2003076584907.
  9. Boucher, Craig J.; Marshall, Paul N.; Novotney, David B.. Ordnance firing system. USP2005056889610.
  10. Folsom,Mark; Piper, III,Charles; Fahey,Wm. David; McGowan,Jared M.. Projectile diverter. USP2006027004423.
  11. Gnemmi,Patrick; Charon,Romain; Samirant,Michel. Projectile steering by plasma discharge. USP2006027002126.
  12. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  13. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  14. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.

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