GB857540A - Arrangement for the guidance control of jet-propelled missiles and aircraft - Google Patents

Arrangement for the guidance control of jet-propelled missiles and aircraft

Info

Publication number
GB857540A
GB857540A GB1464256A GB1464256A GB857540A GB 857540 A GB857540 A GB 857540A GB 1464256 A GB1464256 A GB 1464256A GB 1464256 A GB1464256 A GB 1464256A GB 857540 A GB857540 A GB 857540A
Authority
GB
United Kingdom
Prior art keywords
tube
jet
fins
aircraft
propelled
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
GB1464256A
Inventor
James White Dalgleish
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 GB1464256A priority Critical patent/GB857540A/en
Publication of GB857540A publication Critical patent/GB857540A/en
Expired 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

857,540. Controlling jet-propelled aircraft. PYE Ltd. May 10, 1957 [May 10, 1956], No. 14642/56. Class 4. To control the flight of a jet-propelled missile or aircraft 3, a jet-deflecting tube 1 is pivotally mounted behind the venturi nozzle 2 to turn about an axis near its front. The tube carries spindles 4 turning in bearings 5 so that as the tube is deflected fins 6, which are in the airstream of the missile and carried by the spindles, are turned in such a way that the forces on the fins due to the airstream tend to turn the tube in the direction of deflection. The tube 1 may be mounted for universal movement, in which case bwo fins 7 are arranged at right angles to fins 6, the four fins being coupled to the tube by gimbals.
GB1464256A 1956-05-10 1956-05-10 Arrangement for the guidance control of jet-propelled missiles and aircraft Expired GB857540A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1464256A GB857540A (en) 1956-05-10 1956-05-10 Arrangement for the guidance control of jet-propelled missiles and aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1464256A GB857540A (en) 1956-05-10 1956-05-10 Arrangement for the guidance control of jet-propelled missiles and aircraft

Publications (1)

Publication Number Publication Date
GB857540A true GB857540A (en) 1960-12-29

Family

ID=10044938

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1464256A Expired GB857540A (en) 1956-05-10 1956-05-10 Arrangement for the guidance control of jet-propelled missiles and aircraft

Country Status (1)

Country Link
GB (1) GB857540A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3236182A (en) * 1964-06-03 1966-02-22 Werner K Dahm Air vanes of low hinge moments
US4867393A (en) * 1988-08-17 1989-09-19 Morton Thiokol, Inc. Reduced fin span thrust vector controlled pulsed tactical missile
CN114295014A (en) * 2021-12-30 2022-04-08 宁波天擎航天科技有限公司 Rocket of external rudder system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3236182A (en) * 1964-06-03 1966-02-22 Werner K Dahm Air vanes of low hinge moments
US4867393A (en) * 1988-08-17 1989-09-19 Morton Thiokol, Inc. Reduced fin span thrust vector controlled pulsed tactical missile
CN114295014A (en) * 2021-12-30 2022-04-08 宁波天擎航天科技有限公司 Rocket of external rudder system
CN114295014B (en) * 2021-12-30 2024-03-19 宁波天擎航天科技有限公司 Rocket of external rudder system

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