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GB201205912D0 - Small missile - Google Patents

Small missile

Info

Publication number
GB201205912D0
GB201205912D0 GBGB1205912.7A GB201205912A GB201205912D0 GB 201205912 D0 GB201205912 D0 GB 201205912D0 GB 201205912 A GB201205912 A GB 201205912A GB 201205912 D0 GB201205912 D0 GB 201205912D0
Authority
GB
United Kingdom
Prior art keywords
small missile
missile
small
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.)
Granted
Application number
GBGB1205912.7A
Other versions
GB2489611B (en
GB2489611B8 (en
GB2489611A (en
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.)
LFK Lenkflugkoerpersysteme GmbH
Original Assignee
LFK Lenkflugkoerpersysteme GmbH
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 LFK Lenkflugkoerpersysteme GmbH filed Critical LFK Lenkflugkoerpersysteme GmbH
Publication of GB201205912D0 publication Critical patent/GB201205912D0/en
Publication of GB2489611A publication Critical patent/GB2489611A/en
Publication of GB2489611B publication Critical patent/GB2489611B/en
Application granted granted Critical
Publication of GB2489611B8 publication Critical patent/GB2489611B8/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F42B15/01—Arrangements thereon for guidance or control
    • 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
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/10—Missiles having a trajectory only in the air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F42B33/001—Devices or processes for assembling ammunition, cartridges or cartridge elements from parts

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Manufacturing & Machinery (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
GB1205912.7A 2011-04-01 2012-04-02 Small missile Active GB2489611B8 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102011015780A DE102011015780A1 (en) 2011-04-01 2011-04-01 Small aircraft

Publications (4)

Publication Number Publication Date
GB201205912D0 true GB201205912D0 (en) 2012-05-16
GB2489611A GB2489611A (en) 2012-10-03
GB2489611B GB2489611B (en) 2014-11-19
GB2489611B8 GB2489611B8 (en) 2014-12-03

Family

ID=46160220

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1205912.7A Active GB2489611B8 (en) 2011-04-01 2012-04-02 Small missile

Country Status (3)

Country Link
DE (1) DE102011015780A1 (en)
FR (1) FR2973499B1 (en)
GB (1) GB2489611B8 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112781448A (en) * 2020-12-29 2021-05-11 哈尔滨工程大学 Anti-submarine missile based on water inlet buffer device and control method
CN118242941A (en) * 2024-05-24 2024-06-25 中科华控航天科技合肥有限公司 Winding arc type missile wing furling and loading device

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2581097C1 (en) * 2015-02-19 2016-04-10 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Rocket section with stabilising device of projectile
DE102015012970A1 (en) * 2015-10-07 2017-04-13 Mbda Deutschland Gmbh Function-oriented and reconfigurable missile
DE102023003108A1 (en) * 2023-07-28 2025-01-30 BAYERN-CHEMIE Gesellschaft für flugchemische Antriebe mit beschränkter Haftung TURBINELESS JET ENGINE

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3065929A (en) * 1956-05-15 1962-11-27 Jr Raymond Prunty Holland Aircraft having aerodynamically tiltable thrust
DE1097283B (en) * 1958-09-16 1961-01-12 Messerschmitt Ag Manned or unmanned aircraft with jet propulsion for vertical take-off and landing on the stern on unprepared places
DE2904749C2 (en) * 1979-02-08 1984-01-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Missile in the manner of a drone
DE3643823A1 (en) * 1986-12-20 1988-06-30 Messerschmitt Boelkow Blohm THROTTLE VECTOR CONTROL FOR AIRCRAFT
ES2008200A6 (en) * 1987-09-02 1989-07-16 Munoz Saiz Manuel Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft
US6295932B1 (en) * 1999-03-15 2001-10-02 Lockheed Martin Corporation Electronic safe arm and fire device
DE10303189A1 (en) * 2003-01-27 2004-07-29 Schamuhn, Jörg, Dipl.-Ing. Propeller for model airplane, has impeller which covers cardan shaft housing in direction parallel to longitudinal axis of airplane, with rotor rotatably mounted in housing, and a drive motor to drive the rotor via a drive shaft
DE102007012799B3 (en) 2007-03-16 2008-04-30 Lfk-Lenkflugkörpersysteme Gmbh Control device for the production of torques around a longitudinal and transverse axis of a small missile driven over a steering electronics by propellers, comprises wings having an aerodynamic flight stabilization rudder-fin
DE102008022289B4 (en) * 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. missile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112781448A (en) * 2020-12-29 2021-05-11 哈尔滨工程大学 Anti-submarine missile based on water inlet buffer device and control method
CN118242941A (en) * 2024-05-24 2024-06-25 中科华控航天科技合肥有限公司 Winding arc type missile wing furling and loading device

Also Published As

Publication number Publication date
FR2973499B1 (en) 2019-05-24
GB2489611B (en) 2014-11-19
GB2489611B8 (en) 2014-12-03
GB2489611A (en) 2012-10-03
DE102011015780A1 (en) 2012-10-04
FR2973499A1 (en) 2012-10-05

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