GB847058A - Improvements in rockets and suspending and launching means therefor - Google Patents

Improvements in rockets and suspending and launching means therefor

Info

Publication number
GB847058A
GB847058A GB29065/58A GB2906558A GB847058A GB 847058 A GB847058 A GB 847058A GB 29065/58 A GB29065/58 A GB 29065/58A GB 2906558 A GB2906558 A GB 2906558A GB 847058 A GB847058 A GB 847058A
Authority
GB
United Kingdom
Prior art keywords
rocket
pin
ring
arm
enters
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
GB29065/58A
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.)
Brevets Aero Mecaniques SA
Original Assignee
Brevets Aero Mecaniques 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 Brevets Aero Mecaniques SA filed Critical Brevets Aero Mecaniques SA
Publication of GB847058A publication Critical patent/GB847058A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/10Initiators therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/04Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/052Means for securing the rocket in the launching apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/06Rocket or torpedo launchers for rockets from aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automatic Assembly (AREA)

Abstract

847,058. Suspending and launching rockets. BREVETS AERO-MECANIQUES S.A. Sept. 10, 1958 [Sept. 28, 1957], No. 29065/58. Class 9(2). In a cluster of rockets suspended as described in Specification 846,246, each rocket has two circumferential screwed rings 14 and 15 (Fig. 7), abutting respectively on the slidable tail unit 3 and an abutment on the rocket body which may take the form of a boss 16 which enters into a keyway 17 in ring 14. By unscrewing the ring 15 from the ring 14 (advantageously with a torque wrench), axial play in the assembly is taken up. One ring (preferably 15) may be of plastic in order to introduce a locking effect. The rear suspension may consist of a pin 9 (Fig. 4) which enters into an arm 10 pivoting on a pin 11 in the rocket I. Pin 9 and arm 10 are locked together by a locking pin 12 which is secured in, and acts as a fulcrum for, a flap 5 which enters the nozzle of the lower rocket II. When rocket II is fired, flap 5 is urged rearward by the propellent gases unlocking arm 10 of rocket I from the pin 9 of rocket II. A spring 13 maintains pin 12 in the locked position and also urges arm 10 to the retracted position after unlocking. Specifications 610,685, 738,870, 769,139, and 827,125 also are referred to.
GB29065/58A 1957-09-28 1958-09-10 Improvements in rockets and suspending and launching means therefor Expired GB847058A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
LU350195X 1957-09-28

Publications (1)

Publication Number Publication Date
GB847058A true GB847058A (en) 1960-09-07

Family

ID=19732624

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29065/58A Expired GB847058A (en) 1957-09-28 1958-09-10 Improvements in rockets and suspending and launching means therefor

Country Status (4)

Country Link
CH (1) CH350195A (en)
FR (1) FR1211023A (en)
GB (1) GB847058A (en)
LU (1) LU35482A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB958943A (en) * 1960-02-27 1964-05-27 Brevets Aero Mecaniques Improvements in rockets carried in clusters by a launching machine and in particularan aircraft

Also Published As

Publication number Publication date
FR1211023A (en) 1960-03-11
LU35482A1 (en)
CH350195A (en) 1960-11-15

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