GB827299A - Improvements in or relating to guided missiles - Google Patents

Improvements in or relating to guided missiles

Info

Publication number
GB827299A
GB827299A GB1981756A GB1981756A GB827299A GB 827299 A GB827299 A GB 827299A GB 1981756 A GB1981756 A GB 1981756A GB 1981756 A GB1981756 A GB 1981756A GB 827299 A GB827299 A GB 827299A
Authority
GB
United Kingdom
Prior art keywords
jacks
valves
atmosphere
guided missiles
swivelling
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.)
Expired
Application number
GB1981756A
Inventor
Thomas James Dorricott
Christopher Lawrence Paice
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.)
Pye Electronic Products Ltd
Original Assignee
Pye Ltd
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 Pye Ltd filed Critical Pye Ltd
Priority to GB1981756A priority Critical patent/GB827299A/en
Publication of GB827299A publication Critical patent/GB827299A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • 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
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Air Bags (AREA)

Abstract

827,299. Controlling guided missiles. PYE Ltd. May 20,1957 [June 26, 1956], No. 19817/56. Class 4. Apparatus for steering a guided missile comprises a plurality of pneumatic jacks D which bear against the forward face of the swivelling jet nozzle C. Each jack communicates at H with the combustion chamber L and, through an adjustable valve J, and aperture G, with atmosphere. To steer the missile one or more valves J are moved from the position shown at the top of the Figure to that shown at the bottom whereby one or more jacks are vented to atmosphere with consequent swivelling of nozzle C. Four jacks are preferably provided but if two are employed, they are set in a rotatable mounting which is rotated to a selected position before the valves J are operated.
GB1981756A 1956-06-26 1956-06-26 Improvements in or relating to guided missiles Expired GB827299A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1981756A GB827299A (en) 1956-06-26 1956-06-26 Improvements in or relating to guided missiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1981756A GB827299A (en) 1956-06-26 1956-06-26 Improvements in or relating to guided missiles

Publications (1)

Publication Number Publication Date
GB827299A true GB827299A (en) 1960-02-03

Family

ID=10135723

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1981756A Expired GB827299A (en) 1956-06-26 1956-06-26 Improvements in or relating to guided missiles

Country Status (1)

Country Link
GB (1) GB827299A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2444805A1 (en) * 1978-12-20 1980-07-18 Europ Propulsion Variable angle jet propulsion plant - has pistons in movable nozzle controlled by position of valves in gas line
EP0079653A1 (en) * 1981-11-13 1983-05-25 Philips Norden AB Bi-axial suspension arrangement of a component part in a projectile
US4913379A (en) * 1988-02-23 1990-04-03 Japan as represented by Director General, Technical Research and Development Institute, Japan Defence Agency Rocket flight direction control system
FR2841939A1 (en) * 2002-07-04 2004-01-09 Snecma Propulsion Solide MOBILE DIVERGENT ADJUSTABLE NOZZLE ON CARDAN FOR ROCKET ENGINE

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2444805A1 (en) * 1978-12-20 1980-07-18 Europ Propulsion Variable angle jet propulsion plant - has pistons in movable nozzle controlled by position of valves in gas line
EP0079653A1 (en) * 1981-11-13 1983-05-25 Philips Norden AB Bi-axial suspension arrangement of a component part in a projectile
US4913379A (en) * 1988-02-23 1990-04-03 Japan as represented by Director General, Technical Research and Development Institute, Japan Defence Agency Rocket flight direction control system
FR2841939A1 (en) * 2002-07-04 2004-01-09 Snecma Propulsion Solide MOBILE DIVERGENT ADJUSTABLE NOZZLE ON CARDAN FOR ROCKET ENGINE
WO2004005690A1 (en) * 2002-07-04 2004-01-15 Snecma Propulsion Solide Swivelling nozzle for a rocket engine
NO338429B1 (en) * 2002-07-04 2016-08-15 Herakles Swivel nozzle for a rocket engine.

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