GB955640A - Guided missile - Google Patents
Guided missileInfo
- 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
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.
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)
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)
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)
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 |
-
1954
- 1954-10-18 US US462743A patent/US3132590A/en not_active Expired - Lifetime
-
1955
- 1955-03-07 GB GB6697/55A patent/GB955640A/en not_active Expired
Cited By (2)
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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