NO162583C - Frakoplingsbar skyvekraft-vektormekanisme for et missil. - Google Patents

Frakoplingsbar skyvekraft-vektormekanisme for et missil.

Info

Publication number
NO162583C
NO162583C NO863455A NO863455A NO162583C NO 162583 C NO162583 C NO 162583C NO 863455 A NO863455 A NO 863455A NO 863455 A NO863455 A NO 863455A NO 162583 C NO162583 C NO 162583C
Authority
NO
Norway
Prior art keywords
disconnectable
missile
vector mechanism
pushing vector
pushing
Prior art date
Application number
NO863455A
Other languages
English (en)
Other versions
NO863455D0 (no
NO162583B (no
Inventor
John R Peoples
Billy R Phillips
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of NO863455D0 publication Critical patent/NO863455D0/no
Publication of NO162583B publication Critical patent/NO162583B/no
Publication of NO162583C publication Critical patent/NO162583C/no

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645—Separators
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Control Devices (AREA)
  • Details Of Aerials (AREA)
  • Transmission Devices (AREA)
NO863455A 1985-11-25 1986-08-28 Frakoplingsbar skyvekraft-vektormekanisme for et missil. NO162583C (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US80144585A 1985-11-25 1985-11-25

Publications (3)

Publication Number Publication Date
NO863455D0 NO863455D0 (no) 1986-08-28
NO162583B NO162583B (no) 1989-10-09
NO162583C true NO162583C (no) 1990-01-17

Family

ID=25181115

Family Applications (1)

Application Number Title Priority Date Filing Date
NO863455A NO162583C (no) 1985-11-25 1986-08-28 Frakoplingsbar skyvekraft-vektormekanisme for et missil.

Country Status (6)

Country Link
EP (1) EP0227211B1 (no)
JP (1) JP2593454B2 (no)
KR (1) KR930002105B1 (no)
DE (1) DE3678542D1 (no)
IL (1) IL79864A (no)
NO (1) NO162583C (no)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2272047B (en) * 1989-12-14 1994-07-27 British Aerospace Stand-off weapons
IL115749A (en) * 1994-10-27 2000-02-29 Thomson Csf Missile launching and orientating system
DE19828645C1 (de) * 1998-06-26 1999-11-18 Buck Werke Gmbh & Co I K Flugkörper zur Bekämpfung feststehender und/oder beweglicher Ziele
KR101159648B1 (ko) * 2011-07-29 2012-06-25 삼성탈레스 주식회사 제트엔진이 탑재된 미사일 기만기
FR2997179B1 (fr) * 2012-10-22 2015-01-16 Roxel France Dispositif combine de pilotage de trajectoire et de reduction de trainee.
WO2023152484A1 (en) * 2022-02-10 2023-08-17 Mbda Uk Limited Apparatus for providing an interface between a missile and a launch platform

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1125143A (fr) * 1955-04-27 1956-10-24 Artifices Titan Soc D Fusée à propulseur larguable
US3224370A (en) * 1959-07-27 1965-12-21 Curtiss Wright Corp Booster rocket
US3067682A (en) * 1960-02-18 1962-12-11 Aerojet General Co Gyro pull rocket
GB1269272A (en) * 1968-06-06 1972-04-06 Messeschmitt Bolkow Blohm Gmbh Improvements in multi-stage rockets
US4044970A (en) * 1975-08-08 1977-08-30 General Dynamics Corporation Integrated thrust vector aerodynamic control surface
DE2721656A1 (de) 1977-05-13 1978-11-16 Ver Flugtechnische Werke Stellanordnung zur steuerung von flugkoerpern
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
DE3133339A1 (de) * 1981-08-22 1983-03-10 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen "unbemannter, aus einem transportbehaelter zu startender flugkoerper"

Also Published As

Publication number Publication date
NO863455D0 (no) 1986-08-28
DE3678542D1 (de) 1991-05-08
NO162583B (no) 1989-10-09
KR870005231A (ko) 1987-06-05
IL79864A (en) 1994-05-30
EP0227211B1 (en) 1991-04-03
JPS62125300A (ja) 1987-06-06
JP2593454B2 (ja) 1997-03-26
KR930002105B1 (ko) 1993-03-26
IL79864A0 (en) 1986-11-30
EP0227211A1 (en) 1987-07-01

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Legal Events

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MM1K Lapsed by not paying the annual fees

Free format text: LAPSED IN FEBRUARY 2003