GB9618126D0 - Thruster pack for missile control - Google Patents

Thruster pack for missile control

Info

Publication number
GB9618126D0
GB9618126D0 GBGB9618126.8A GB9618126A GB9618126D0 GB 9618126 D0 GB9618126 D0 GB 9618126D0 GB 9618126 A GB9618126 A GB 9618126A GB 9618126 D0 GB9618126 D0 GB 9618126D0
Authority
GB
United Kingdom
Prior art keywords
thruster
pack
missile control
missile
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
GBGB9618126.8A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by British Aerospace PLC filed Critical British Aerospace PLC
Priority to GBGB9618126.8A priority Critical patent/GB9618126D0/en
Publication of GB9618126D0 publication Critical patent/GB9618126D0/en
Priority to GB9717839A priority patent/GB2316663A/en
Priority to FR9710754A priority patent/FR2753432A1/en
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GBGB9618126.8A 1996-08-29 1996-08-29 Thruster pack for missile control Pending GB9618126D0 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GBGB9618126.8A GB9618126D0 (en) 1996-08-29 1996-08-29 Thruster pack for missile control
GB9717839A GB2316663A (en) 1996-08-29 1997-08-26 Thruster pack for missile control
FR9710754A FR2753432A1 (en) 1996-08-29 1997-08-28 PUSH-BODY MECHANISM FOR ATTITUDE CONTROL OF A FLYING BODY

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9618126.8A GB9618126D0 (en) 1996-08-29 1996-08-29 Thruster pack for missile control

Publications (1)

Publication Number Publication Date
GB9618126D0 true GB9618126D0 (en) 1997-01-08

Family

ID=10799175

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9618126.8A Pending GB9618126D0 (en) 1996-08-29 1996-08-29 Thruster pack for missile control
GB9717839A Withdrawn GB2316663A (en) 1996-08-29 1997-08-26 Thruster pack for missile control

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB9717839A Withdrawn GB2316663A (en) 1996-08-29 1997-08-26 Thruster pack for missile control

Country Status (2)

Country Link
FR (1) FR2753432A1 (en)
GB (2) GB9618126D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113654412A (en) * 2021-09-13 2021-11-16 北京理工大学 Pulse thrust attitude control device driven by motor

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6178741B1 (en) * 1998-10-16 2001-01-30 Trw Inc. Mems synthesized divert propulsion system
US6308911B1 (en) * 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US7851732B2 (en) * 2006-03-07 2010-12-14 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US8173946B1 (en) 2008-08-26 2012-05-08 Raytheon Company Method of intercepting incoming projectile
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
IL269920B2 (en) * 2019-10-10 2024-10-01 Israel Aerospace Ind Ltd Projectile trajectory shaping

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1605295A (en) * 1967-12-13 1988-06-08 Secr Defence Rocket projectiles
EP0371007A3 (en) * 1985-11-22 1991-04-17 Ship Systems, Inc. Spin-stabilized projectile with pulse receiver and method of use
US4844380A (en) * 1985-11-25 1989-07-04 Hughes Aircraft Company Detachable thrust vector mechanism for an aeronautical vehicle
GB8618510D0 (en) * 1986-07-29 1986-12-17 Imi Kynuch Ltd Guidance apparatus for projectiles
FR2686687B1 (en) * 1987-04-22 1994-05-13 Thomson Brandt Armements METHOD AND DEVICE FOR DRIVING A PROJECTILE ACCORDING TO ITS THREE AXES OF ROLL TANGAGE AND LACE.
US4899956A (en) * 1988-07-20 1990-02-13 Teleflex, Incorporated Self-contained supplemental guidance module for projectile weapons
DE4408085C2 (en) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Device for guiding a missile not rotating about its longitudinal axis
US5819478A (en) 1994-03-14 1998-10-13 D. Anderson And Son Limited Damp-proof course member

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113654412A (en) * 2021-09-13 2021-11-16 北京理工大学 Pulse thrust attitude control device driven by motor

Also Published As

Publication number Publication date
GB9717839D0 (en) 1997-10-29
FR2753432A1 (en) 1998-03-20
GB2316663A (en) 1998-03-04

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Legal Events

Date Code Title Description
730 Substitution of applicants allowed (sect. 30/1977)