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GB982779A - Improvements in or relating to aerial vehicles - Google Patents

Improvements in or relating to aerial vehicles

Info

Publication number
GB982779A
GB982779A GB2657962A GB2657962A GB982779A GB 982779 A GB982779 A GB 982779A GB 2657962 A GB2657962 A GB 2657962A GB 2657962 A GB2657962 A GB 2657962A GB 982779 A GB982779 A GB 982779A
Authority
GB
United Kingdom
Prior art keywords
missile
july
longitudinal axis
fins
wings
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
GB2657962A
Inventor
Mansel Edward David
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.)
English Electric Co Ltd
Original Assignee
English Electric Co 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 English Electric Co Ltd filed Critical English Electric Co Ltd
Priority to GB2657962A priority Critical patent/GB982779A/en
Publication of GB982779A publication Critical patent/GB982779A/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
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins
    • 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

982,779. Self-propelled missiles. ENGLISH ELECTRIC CO. Ltd. July 8, 1963 [July 10, 1962], No. 26579/62. Heading F3A. [Also in Division B7] An aerial vehicle, such as a missile, has movable wings 15 fitted on its forward or central part, and a stabilizer mounted aft of the wings for free rotation about the longitudinal axis of the vehicle and having at least three fixed incidence stabilizing fins 17 each mounted in a plane radial to the longitudinal axis. As described, there are four fins 17 fixed to a sleeve 18 mounted by ball-bearings on the rear end of the missile which is divided into compartments containing radar equipment 11, guidance and control equipment 12, the useful load or warhead 13, and a solid fuel rocket motor 14 having an exhaust nozzle 16.
GB2657962A 1962-07-10 1962-07-10 Improvements in or relating to aerial vehicles Expired GB982779A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2657962A GB982779A (en) 1962-07-10 1962-07-10 Improvements in or relating to aerial vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2657962A GB982779A (en) 1962-07-10 1962-07-10 Improvements in or relating to aerial vehicles

Publications (1)

Publication Number Publication Date
GB982779A true GB982779A (en) 1965-02-10

Family

ID=10245853

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2657962A Expired GB982779A (en) 1962-07-10 1962-07-10 Improvements in or relating to aerial vehicles

Country Status (1)

Country Link
GB (1) GB982779A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2096658A1 (en) * 1970-05-05 1972-02-25 Even Claude
US5207397A (en) * 1990-06-08 1993-05-04 Eidetics International, Inc. Rotatable nose and nose boom strakes and methods for aircraft stability and control
WO1994016286A1 (en) * 1993-01-14 1994-07-21 Erno Raumfahrttechnik Gmbh Control device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2096658A1 (en) * 1970-05-05 1972-02-25 Even Claude
US5207397A (en) * 1990-06-08 1993-05-04 Eidetics International, Inc. Rotatable nose and nose boom strakes and methods for aircraft stability and control
WO1994016286A1 (en) * 1993-01-14 1994-07-21 Erno Raumfahrttechnik Gmbh Control device
US5593110A (en) * 1993-01-14 1997-01-14 Daimler-Benz Aerospace Ag Apparatus for controlling the structural dynamic response of a rocket

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