GB923829A - Improvements in or relating to missiles with stabilizing wings having a high ballistic reliability - Google Patents

Improvements in or relating to missiles with stabilizing wings having a high ballistic reliability

Info

Publication number
GB923829A
GB923829A GB4298060A GB4298060A GB923829A GB 923829 A GB923829 A GB 923829A GB 4298060 A GB4298060 A GB 4298060A GB 4298060 A GB4298060 A GB 4298060A GB 923829 A GB923829 A GB 923829A
Authority
GB
United Kingdom
Prior art keywords
nozzles
wings
head element
missiles
secured
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
GB4298060A
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.)
Les Forges de Zeebrugge SA
Original Assignee
Les Forges de Zeebrugge SA
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 Les Forges de Zeebrugge SA filed Critical Les Forges de Zeebrugge SA
Publication of GB923829A publication Critical patent/GB923829A/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
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles

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

923,829. Self-propelled missiles with stabilizing wings. FORGES DE ZEEBRUGGE S.A. Dec. 14, 1960 [July 13, 1960], No. 42980/60. Classes 9 (1) and 9 (2). A self - propelled missile comprises a motor tube 1 at the tail end of which is secured a head element 2 made in one piece and carrying nozzles 14 which are forced into position from the interior of the element 2, the latter having a tubular projection 18 used as a guiding means for a device to deploy the stabilizing fins. The four nozzles 14 fit into four cylindrical openings 13 of stepped bore in the single head element 2 and are held firmly against inner shoulders 15 by the pressure of the propellant gases so that the nozzles 14 are accurately positioned during flight. A rigid fit with the element 2 is ensured by providing securing points 17. Within the element 2 is a tubular projection 18 in which is engaged the rod 19 driving the cross-shaped pushing device 28 in spreading the folded wings 7: the device 28 then forms a holding stop as in Fig. 3. A cap 8 engaging a shoulder of the head element 2 entirely covers the folded wings 7 which are secured to each other by a plate 9 fitting in the end slot 10 of each wing. An elastic element 11 is compressed between the plate 9 and the slots 10.
GB4298060A 1960-07-13 1960-12-14 Improvements in or relating to missiles with stabilizing wings having a high ballistic reliability Expired GB923829A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE39903 1960-07-13

Publications (1)

Publication Number Publication Date
GB923829A true GB923829A (en) 1963-04-18

Family

ID=3840198

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4298060A Expired GB923829A (en) 1960-07-13 1960-12-14 Improvements in or relating to missiles with stabilizing wings having a high ballistic reliability

Country Status (1)

Country Link
GB (1) GB923829A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1203647B (en) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Fin tail, especially for rocket projectiles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1203647B (en) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Fin tail, especially for rocket projectiles

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