GB1311747A - Missile - Google Patents

Missile

Info

Publication number
GB1311747A
GB1311747A GB2737770A GB2737770A GB1311747A GB 1311747 A GB1311747 A GB 1311747A GB 2737770 A GB2737770 A GB 2737770A GB 2737770 A GB2737770 A GB 2737770A GB 1311747 A GB1311747 A GB 1311747A
Authority
GB
United Kingdom
Prior art keywords
missile
wings
gravity
nozzles
centre
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
GB2737770A
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.)
Saab Bofors AB
Original Assignee
Bofors AB
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 Bofors AB filed Critical Bofors AB
Publication of GB1311747A publication Critical patent/GB1311747A/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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/70—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

Abstract

1311747 Missiles BOFORS AB 5 June 1970 [6 June 1969] 27377/70 Heading F3A A missile comprises solid fuel charges 2 and 3 whose common centre of gravity substantially coincides with the total centre of gravity of the missile and the combustion gases from which pass to a plurality of nozzles 7 which are mounted in an annular member 5, stabilizing wings 6 being alternately attached to the annular member 5 between adjacent nozzles. The wings can be folded alongside the missile. Both the wings and nozzles are mounted in a plurality of individual recesses 8 or in a common annular recess. The wings are preferably mounted close to the total centre of gravity and the resultant of the thrust from the nozzles coincides with the axis of symmetry of the missile and is directed through the total centre of gravity.
GB2737770A 1969-06-06 1970-06-05 Missile Expired GB1311747A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE08063/69A SE340417B (en) 1969-06-06 1969-06-06

Publications (1)

Publication Number Publication Date
GB1311747A true GB1311747A (en) 1973-03-28

Family

ID=20273043

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2737770A Expired GB1311747A (en) 1969-06-06 1970-06-05 Missile

Country Status (10)

Country Link
US (1) US3684215A (en)
JP (1) JPS4810360B1 (en)
BE (1) BE751547A (en)
CH (1) CH508863A (en)
DE (1) DE2027371C3 (en)
FR (1) FR2049166B1 (en)
GB (1) GB1311747A (en)
NL (1) NL161255C (en)
NO (1) NO125748B (en)
SE (1) SE340417B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172383A (en) * 1981-06-04 1986-09-17 Aerospatiale Guided missile system

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463909B1 (en) * 1979-08-17 1985-10-25 Thomson Brandt METHOD OF PILOTING AND GUIDING A MISSILE, AND MISSILE PROVIDED WITH MEANS FOR IMPLEMENTING THIS METHOD
FR2500149B1 (en) * 1981-02-17 1985-12-06 Poudres & Explosifs Ste Nale PROPULSIVE LOADING BIREGIME WITH TRUMPET HAVING A STAR SECTION
FR2578665B1 (en) * 1981-06-04 1988-02-12 Aerospatiale LOW SPEED MISSILE PILOTING METHOD, WEAPON AND MISSILE SYSTEM FOR IMPLEMENTING THE METHOD
FR2863665B1 (en) * 1988-10-12 2007-03-30 Aerospatiale STATOREACTOR HAVING A TUBULAR AND MISSILE STRUCTURE PROPULATED BY SUCH STATOREACTOR
IL101730A (en) * 1992-04-30 1995-12-31 Israel State Moving body such as missile having wings erectable upon acceleration
US8350200B1 (en) * 2009-03-26 2013-01-08 Lockheed Martin Corporation Passive aerosurface adjustment for static margin management
CN108562195B (en) * 2018-01-12 2019-05-24 北京航空航天大学 A kind of modularization counter weight device and rocket being conveniently adjusted

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB594516A (en) * 1940-09-04 1947-11-13 Charles Dennistoun Burney Improvements in or relating to projectiles operating with rocket propulsion
US2503271A (en) * 1945-02-06 1950-04-11 Clarence N Hickman Rocket projectile
US2816721A (en) * 1953-09-15 1957-12-17 Taylor Richard John Rocket powered aerial vehicle
US3013494A (en) * 1957-08-09 1961-12-19 Chanut Pierre Louis Jean Guided missile
US3127838A (en) * 1960-10-12 1964-04-07 Bombrini Parodi Delfino Spa Retractable blade tail unit for projectiles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172383A (en) * 1981-06-04 1986-09-17 Aerospatiale Guided missile system

Also Published As

Publication number Publication date
JPS4810360B1 (en) 1973-04-02
DE2027371C3 (en) 1980-01-03
NL161255B (en) 1979-08-15
CH508863A (en) 1971-06-15
DE2027371B2 (en) 1979-05-03
NL161255C (en) 1980-01-15
BE751547A (en) 1970-11-16
SE340417B (en) 1971-11-15
FR2049166A1 (en) 1971-03-26
DE2027371A1 (en) 1970-12-10
NL7007998A (en) 1970-12-08
US3684215A (en) 1972-08-15
FR2049166B1 (en) 1974-05-24
NO125748B (en) 1972-10-23

Similar Documents

Publication Publication Date Title
GB1510986A (en) Projectile with an ejectable payload
GB1449560A (en) Thermal detonation energy-initiatable blasting caps and detonation system and method
GB1428412A (en) Solid fuel rocket motors
ES476388A1 (en) Anti-aircraft projectile.
GB1165802A (en) Improved Rifle Grenade
GB1311747A (en) Missile
GB1216823A (en) Solid fuel rocket engine
GB1461686A (en) Housings for missile warheads
GB1199239A (en) Improvements in or relating to a Projectile Having a Combustible Charge Arranged to be Released at a Point on the Projectile Trajectory
GB1321588A (en) Spinstabilised rocket-propelled projectile
GB1430750A (en) Fragmentation warhead for use in missiles
GB1205167A (en) Improvements in or relating to armour-piercing shells
GB1245707A (en) Solid propellant rocket engine
GB1278021A (en) Improvements in or relating to projectiles
GB1120391A (en) Improvements in or relating to rocketwise propelled projectiles
GB941430A (en) Improvements in rockets
GB1354932A (en) Splinter-forming encased explosive bodies
GB1085045A (en) A projectile or aerial bomb
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
GB1315723A (en) Pyrotechnical illuminating body with light emission
GB1379963A (en) Ignitable charge device for ejection from a carrier such as a rocket or projectile
GB953080A (en) Improvements in or relating to rocketwise propelled projectiles of the unguided type
GB1513745A (en) Artillery pilot rocket
GB975086A (en) Improvements in or relating to projectiles
GB1465259A (en) Explosive devices

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee