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Propulsion/control modular booster

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/02    F42B-015/12    F02K-001/20   
미국특허분류(USC) 244/322 ; 60/230 ; 102/378
출원번호 US-0184823 (1980-09-08)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 12  인용 특허 : 3
초록

A modular, apogee-control package is disclosed which can be added to existing missiles, and which will limit the apogee of the missile trajectory by implementation of thrust vector control (TVC). The package comprises a boost guidance unit, a solid rocket propellant motor, and jet vane TVC.

대표
청구항
▼

An apparatus for apogee-controlled launch of a guided missile comprising: boost means for variably controlling said guided missile at launch having fore and aft ends with a thrust termination port in the aft end of said boost means; clamping means for removably attaching said boost means\fore end to the aft end of said guided missile, said clamping means sequentially connected to said thrust termination port such that after said clamping means releases said thrust termination port is activated; a rocket motor and propellant fixedly housed inside said boo...

이 특허에 인용된 특허 (3)

  1. Bastian Thomas W. (Fullerton CA). Jet tab control mechanism for thrust vector control. USP1981064274610.
  2. Takahashi ; Kentaro ; Urano ; Shigeru. Method of producing ferrous sintered alloy of improved wear resistance. USP1978104123265.
  3. Rotmans ; Richard J.. Thrust vector control actuation system. USP1978124131246.

이 특허를 인용한 특허 피인용횟수: 12

  1. Ransom Stephen (Stuhr DEX) Relotius Klaus-Dieter (Bremen DEX). Apparatus for controlling the structural dynamic response of a rocket. USP1997015593110.
  2. Danielson, Arnold O.. Integrated aerodynamic fin and stowable TVC vane system. USP1994065320304.
  3. Caye, Paul; Caillaud, James; Laporte, Guillaume. Method and system for piloting a flying craft with rear propulsion unit. USP2014098825231.
  4. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  5. Roland Gauggel DE; Michael Arnold DE; Reinhard Kruger DE; Norbert Tranapp DE. Missile for combating stationary and/or moving targets. USP2002106462322.
  6. Arkhangelsky Ivan Ivanovitch,RUX ; Bolotov Eugene Gueorguevitch,RUX ; Philippov Vladimir Sergueevitch,RUX ; Mizrokhi Vladimir Yakovlevitch,RUX ; Svetlov Vladimir Grigorievitch,RUX ; Stanevsky Gregory. Missile launching and orientation system. USP1998105823469.
  7. Anderson,Steven E.. Modular projectile system. USP2009037506587.
  8. Teetzel, James W.; Celona, Marc J.; Lemire, Gary M.. Modular rocket system. USP2015119194678.
  9. Gobel Gerald W. (Federal Way WA). Passive separation device and method for finned booster. USP1986094614318.
  10. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  11. King Maurice E. (Rancho Palos Verdes CA) Katucki Gregory M. (Harleysville PA). Self-contained supplemental guidance module for projectile weapons. USP1990024899956.
  12. Dillinger, Robert B.; Danielson, Arnold O.. Stowable three-axis reaction-steering system. USP198712H000384.

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