GB955640A - Guided missile - Google Patents

Guided missile

Info

Publication number
GB955640A
GB955640A GB6697/55A GB669755A GB955640A GB 955640 A GB955640 A GB 955640A GB 6697/55 A GB6697/55 A GB 6697/55A GB 669755 A GB669755 A GB 669755A GB 955640 A GB955640 A GB 955640A
Authority
GB
United Kingdom
Prior art keywords
guided missile
attached
flaps
flap portion
fixed
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
GB6697/55A
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.)
Bell Aerospace Corp
Original Assignee
Bell Aerospace 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 Bell Aerospace Corp filed Critical Bell Aerospace Corp
Publication of GB955640A publication Critical patent/GB955640A/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
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Landscapes

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

Abstract

955,640. Aircraft framework and control surfaces. BELL AEROSPACE CORPORATION. March 7, 1955 [Oct. 18, 1954], No. 6697/55. Headings B7G and B7W. [Also in Division F3] A guided missile is provided with four fixed planes 42, of which two are shown in Fig. 5, at right angles to each other, and with movable control flaps 46 attached to each fixed plane. Each flap 46 is bolted by a bolt 66 to a bracket 68 attached to a fixed plane 42 and by bolts 62 to a base flap portion 64; the flaps are thus readily replaceable. The base flap portion 64 is provided with a stub shaft having a splined end 49 which fits into the end of a cross shaft 50; the two cross shafts are cut away, as indicated at 52, so that each is free to rotate through 50 degrees.
GB6697/55A 1954-10-18 1955-03-07 Guided missile Expired GB955640A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US462743A US3132590A (en) 1954-10-18 1954-10-18 Missile with separable components

Publications (1)

Publication Number Publication Date
GB955640A true GB955640A (en) 1964-04-15

Family

ID=23837606

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6697/55A Expired GB955640A (en) 1954-10-18 1955-03-07 Guided missile

Country Status (2)

Country Link
US (1) US3132590A (en)
GB (1) GB955640A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109341440A (en) * 2018-11-14 2019-02-15 中国空空导弹研究院 A kind of and conformal telemetering equipment of guided missile cable radome fairing

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3272124A (en) * 1960-11-28 1966-09-13 Pneumo Dynamics Corp Solid propellant actuation system
US3166014A (en) * 1960-12-27 1965-01-19 Elmer W Travis Separation mechanism
US3229636A (en) * 1964-02-27 1966-01-18 James W Mayo Missile stage separation indicator and stage initiator
US3245351A (en) * 1964-05-15 1966-04-12 Jerry W Crossett Separable connector for an interstage missile
US3373955A (en) * 1964-05-25 1968-03-19 Huska Paul Pitch and yaw actuator assembly for vehicle guidance surfaces
US4098168A (en) * 1970-09-15 1978-07-04 Vereinigte Flugtechnische Werke-Fokker G.M.B.H. Mechanical structure
US3790103A (en) * 1972-08-21 1974-02-05 Us Navy Rotating fin
FR2321723A1 (en) * 1975-07-29 1977-03-18 Thomson Brandt ATTITUDE CONTROL SYSTEM AND MACHINE EQUIPPED WITH SUCH A SYSTEM
DE2827781C2 (en) * 1978-06-24 1985-11-14 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Coupling head for external loads on aircraft
DE2935044A1 (en) * 1979-08-30 1981-03-19 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen UNMANNED MISSILE TO BE LAUNCHED FROM A CONTAINER
US4623106A (en) * 1984-10-25 1986-11-18 The United States Of America As Represented By The Secretary Of The Navy Reentry vehicle having active control and passive design modifications
DE19715972A1 (en) * 1997-04-17 1998-10-22 Bodenseewerk Geraetetech Hook arrangement for missiles
US7709772B1 (en) * 2005-12-02 2010-05-04 Orbital Research Inc. Aircraft, missile, projectile or underwater vehicle with improved control system
US20100212534A1 (en) * 2006-04-10 2010-08-26 Stefan Thiesen Projectile with a flared tailpiece
GB0905027D0 (en) * 2009-03-24 2009-05-06 Allen Technology Ltd Flying apparatus
CN113357962B (en) * 2021-05-19 2023-01-20 上海机电工程研究所 Auxiliary supporting device for restraining radial runout of guided missile

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1547329A (en) * 1923-12-21 1925-07-28 Whitehead Torpedo Company Ltd Automobile torpedo
US2414898A (en) * 1942-06-11 1947-01-28 Rous Bernard Shell
US2413621A (en) * 1944-03-22 1946-12-31 Rca Corp Radio controlled rocket
US2644396A (en) * 1948-10-01 1953-07-07 United Aircraft Corp Aerial missile
US2654320A (en) * 1949-03-07 1953-10-06 Roy J Schmid Severable aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109341440A (en) * 2018-11-14 2019-02-15 中国空空导弹研究院 A kind of and conformal telemetering equipment of guided missile cable radome fairing
CN109341440B (en) * 2018-11-14 2023-10-20 中国空空导弹研究院 Telemetry device conformal with missile cable fairing

Also Published As

Publication number Publication date
US3132590A (en) 1964-05-12

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