GB868408A - Improvements in and relating to an improved nozzle and tailplane device for a self-propelling missile - Google Patents

Improvements in and relating to an improved nozzle and tailplane device for a self-propelling missile

Info

Publication number
GB868408A
GB868408A GB6984/60A GB698460A GB868408A GB 868408 A GB868408 A GB 868408A GB 6984/60 A GB6984/60 A GB 6984/60A GB 698460 A GB698460 A GB 698460A GB 868408 A GB868408 A GB 868408A
Authority
GB
United Kingdom
Prior art keywords
fins
nozzle
missile
support
self
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
GB6984/60A
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.)
Hotchkiss Brandt SA
Original Assignee
Hotchkiss Brandt 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 Hotchkiss Brandt SA filed Critical Hotchkiss Brandt SA
Publication of GB868408A publication Critical patent/GB868408A/en
Expired legal-status Critical Current

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E02—HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02D—FOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D5/00—Bulkheads, piles, or other structural elements specially adapted to foundation engineering
    • E02D5/22—Piles
    • E02D5/58—Prestressed concrete piles
    • 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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Abstract

868,408. Tail assemblies for self-propelled missiles. HOTCHKISS-BRANDT. Feb. 29, 1960 [March 9, 1959], No. 6984/60. Classes 9(1) and 9(2). A fin-stabilized self-propelled missile is provided having fins arranged on transverse pivots and maintained in a collapsed state prior to launching, deployment of the fins being produced by the pressure of the propellent gases. According to the invention the fins A are mounted on a support 1 screwed into the rear of the rocket casing C and having an axial bore in which the Venturi nozzle T is slidable, the nozzle exterior being shaped to provide bearing surfaces for parts of the fins, such that before launching the fins maintain the nozzle in its forward position and after launching the nozzle is thrust rearwardly by the gases and forces the fins to rotate about their pivots 13. The support 1 is counterbored to house a seal 9 around the nozzle and heat-insulating material 10 shielding the support from the propellant D. Radially arranged slots 4 in the support receive the forward ends of the fins of which the pivots 13 are housed in blind bores 5, Fig. 6. Each fin A has a doubly-bevelled edge 14, which becomes the leading edge when the fins are deployed. A band B securing the fins in the collapsed position is forced off when the missile is placed in a launcher. Small vanes 12 inclined to the longitudinal axis of the missile may be placed in the nozzle to produce a rotary motion of the missile. The slots in the support may also be so arranged that, when deployed, the fins A give a spin to the missile.
GB6984/60A 1959-03-09 1960-02-29 Improvements in and relating to an improved nozzle and tailplane device for a self-propelling missile Expired GB868408A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR788779A FR1228212A (en) 1959-03-09 1959-03-09 Advanced rocket nozzle and tail device

Publications (1)

Publication Number Publication Date
GB868408A true GB868408A (en) 1961-05-17

Family

ID=8712208

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6984/60A Expired GB868408A (en) 1959-03-09 1960-02-29 Improvements in and relating to an improved nozzle and tailplane device for a self-propelling missile

Country Status (8)

Country Link
US (1) US3053184A (en)
BE (1) BE587895A (en)
CH (1) CH359066A (en)
DE (1) DE1148160B (en)
ES (1) ES256216A1 (en)
FR (1) FR1228212A (en)
GB (1) GB868408A (en)
NL (2) NL106348C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113237393A (en) * 2021-04-28 2021-08-10 北京星途探索科技有限公司 High-precision stabilizing device

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL266892A (en) * 1960-07-11
DE1203647B (en) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Fin tail, especially for rocket projectiles
DE1199663B (en) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Nozzle for missiles or rocket-like projectiles
FR82955E (en) * 1962-10-05 1964-05-22 Soc Tech De Rech Ind Rocket refinements
US3946638A (en) * 1974-03-29 1976-03-30 The United States Of America As Represented By The Secretary Of The Army Low recoil anti-tank rocket launcher
FR2388243A1 (en) * 1977-04-21 1978-11-17 Europ Propulsion DEVICE FOR GIVING A ROTATIONAL MOVEMENT TO A UNIT WHEN IT IS LAUNCHED
SE444612B (en) * 1984-12-13 1986-04-21 Ffv Affersverket GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL
FR2721702B1 (en) * 1994-06-28 1996-08-14 Luchaire Defense Sa Device for deploying a projectile fin.
CN108007280B (en) * 2017-12-28 2023-08-15 北京威标至远科技发展有限公司 Steering engine heat-proof structure
US20190366362A1 (en) * 2018-06-05 2019-12-05 United Technologies Corporation Cold spray deposition apparatus, system, and method
US11653613B2 (en) 2020-11-02 2023-05-23 Monsanto Technology Llc Soybean variety 01077829
US11547075B2 (en) 2020-11-02 2023-01-10 Monsanto Technology Llc Soybean variety 01078822
US11477960B2 (en) 2020-11-02 2022-10-25 Monsanto Technology Llc Soybean variety 01077912
US11612128B2 (en) 2020-11-02 2023-03-28 Monsanto Technology Llc Soybean variety 01083666
CN112729033B (en) * 2020-12-28 2024-02-23 安徽江南爆破工程有限公司 Heat insulation device for high-temperature blasting and blasting method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR715385A (en) * 1931-08-10 1931-12-02 Folding tail for aviation bombs
FR896502A (en) * 1940-09-23 1945-02-23 Commerciale Caproni Comp Device for controlling the fins of a projectile fitted with a tail unit
BE565999A (en) * 1953-02-06
US2821924A (en) * 1954-07-09 1958-02-04 Lawrence J Hansen Fin stabilized projectile

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113237393A (en) * 2021-04-28 2021-08-10 北京星途探索科技有限公司 High-precision stabilizing device

Also Published As

Publication number Publication date
NL106348C (en)
US3053184A (en) 1962-09-11
BE587895A (en) 1960-06-16
NL248980A (en)
ES256216A1 (en) 1960-08-16
CH359066A (en) 1961-12-15
DE1148160B (en) 1963-05-02
FR1228212A (en) 1960-08-29

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