CH508863A - Missile with stabilizing wings and solid-state propulsion device - Google Patents

Missile with stabilizing wings and solid-state propulsion device

Info

Publication number
CH508863A
CH508863A CH832570A CH832570A CH508863A CH 508863 A CH508863 A CH 508863A CH 832570 A CH832570 A CH 832570A CH 832570 A CH832570 A CH 832570A CH 508863 A CH508863 A CH 508863A
Authority
CH
Switzerland
Prior art keywords
missile
solid
propulsion device
stabilizing wings
state propulsion
Prior art date
Application number
CH832570A
Other languages
German (de)
Inventor
Jacobson Gunnar
Olsson Olof
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 CH508863A publication Critical patent/CH508863A/en

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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
CH832570A 1969-06-06 1970-06-03 Missile with stabilizing wings and solid-state propulsion device CH508863A (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
CH508863A true CH508863A (en) 1971-06-15

Family

ID=20273043

Family Applications (1)

Application Number Title Priority Date Filing Date
CH832570A CH508863A (en) 1969-06-06 1970-06-03 Missile with stabilizing wings and solid-state propulsion device

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)

Families Citing this family (8)

* 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
GB2172383B (en) * 1981-06-04 1987-08-12 Aerospatiale Guided missile system
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

Also Published As

Publication number Publication date
BE751547A (en) 1970-11-16
DE2027371B2 (en) 1979-05-03
DE2027371A1 (en) 1970-12-10
SE340417B (en) 1971-11-15
DE2027371C3 (en) 1980-01-03
FR2049166A1 (en) 1971-03-26
FR2049166B1 (en) 1974-05-24
NL161255C (en) 1980-01-15
US3684215A (en) 1972-08-15
NL7007998A (en) 1970-12-08
NL161255B (en) 1979-08-15
NO125748B (en) 1972-10-23
JPS4810360B1 (en) 1973-04-02
GB1311747A (en) 1973-03-28

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Legal Events

Date Code Title Description
PL Patent ceased