GB1282609A - Improvements in and relating to missile apparatus - Google Patents

Improvements in and relating to missile apparatus

Info

Publication number
GB1282609A
GB1282609A GB56838/69A GB5683869A GB1282609A GB 1282609 A GB1282609 A GB 1282609A GB 56838/69 A GB56838/69 A GB 56838/69A GB 5683869 A GB5683869 A GB 5683869A GB 1282609 A GB1282609 A GB 1282609A
Authority
GB
United Kingdom
Prior art keywords
missile
fuselage
motor
launching
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
GB56838/69A
Inventor
Arthur Moskowitz
William Fraser Macinnes
Calhoun Winfred Sumrall
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.)
Space Systems Loral LLC
Original Assignee
Philco Ford Corp
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 Philco Ford Corp filed Critical Philco Ford Corp
Publication of GB1282609A publication Critical patent/GB1282609A/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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1282609 Self-propelling missile and launching means therefor; rockets PHILCO-FORD CORP 20 Nov 1969 [20 Nov 1968] 56838/69 Heading F3A and F3C A self-propelled missile, for use as a target, and its launching means, comprises a tubular fuselarge section 11 (Fig. 2) fitted over a launching tube 15 and secured thereto by frangible screws which break when a predetermined gas pressure is developed by a launching motor 32. A blast shield 16 is provided on the launching tube. Glass-fibre reinforced plastic fins 13 are secured to the fuselage by straps (17, Fig. 5, not shown) and contain further rocker motors 22 in their base portions. The fins are slightly inclined so as to rotate the missile in flight. The frangible screws 27, Fig. 3, extend between an annular member 33 fastened to the motor 32 and an annular member 31 threaded in an extension 26 of the launching tube. The motor 32 is secured in the fuselage 11 by a clamp 37 which pulls the member 33 against a wooden block 34 fast with the fuselage. The fuselage is made of cardboard lined with a thermally protective layer of aluminium. The motor 32 is electrically ignited and as the missile moves away from the launching tube plugs are withdrawn from an electrical circuit which then ignites the motors 22.
GB56838/69A 1968-11-20 1969-11-20 Improvements in and relating to missile apparatus Expired GB1282609A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US77725068A 1968-11-20 1968-11-20

Publications (1)

Publication Number Publication Date
GB1282609A true GB1282609A (en) 1972-07-19

Family

ID=25109712

Family Applications (1)

Application Number Title Priority Date Filing Date
GB56838/69A Expired GB1282609A (en) 1968-11-20 1969-11-20 Improvements in and relating to missile apparatus

Country Status (4)

Country Link
US (1) US3605549A (en)
DE (1) DE1958355C3 (en)
FR (1) FR2023662A1 (en)
GB (1) GB1282609A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2239695A (en) * 1986-07-01 1991-07-10 Gen Electric A round of ammunition

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1131946A (en) * 1977-09-07 1982-09-21 Donald L. Smith Shear pin release system
US4333382A (en) * 1979-12-26 1982-06-08 The United States Of America As Represented By The Secretary Of The Navy Boost assisted missile launcher
RU2557125C2 (en) * 2013-06-24 2015-07-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева Aft body of aircraft with annular location of jet engine nozzles on its bottom protection (versions)
CN114184091A (en) * 2021-04-08 2022-03-15 西安龙飞电气技术有限公司 Infrared radar dual-mode digital processing method for air-to-air missile seeker
CN113218244A (en) * 2021-05-11 2021-08-06 北京空天技术研究所 Windproof locking mechanism

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2239695A (en) * 1986-07-01 1991-07-10 Gen Electric A round of ammunition
GB2239695B (en) * 1986-07-01 1991-10-23 Gen Electric A round of ammunition.

Also Published As

Publication number Publication date
US3605549A (en) 1971-09-20
DE1958355C3 (en) 1974-08-22
DE1958355B2 (en) 1974-01-24
DE1958355A1 (en) 1970-05-27
FR2023662A1 (en) 1970-08-21

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees