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
Authority: CH; Switzerland
Prior art keywords: missile; solid; propulsion device; stabilizing wings; state propulsion
Prior art date: 1969-06-06

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.)

1969-06-06

Filing date

1970-06-03

Publication date

1971-06-15

1970-06-03 Application filed by Bofors Ab filed Critical Bofors Ab

1971-06-15 Publication of CH508863A publication Critical patent/CH508863A/en

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)
Aviation & Aerospace 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

1969
- 1969-06-06 SE SE08063/69A patent/SE340417B/xx unknown
1970
- 1970-05-28 US US41373A patent/US3684215A/en not_active Expired - Lifetime
- 1970-06-02 NL NL7007998.A patent/NL161255C/en not_active IP Right Cessation
- 1970-06-03 CH CH832570A patent/CH508863A/en not_active IP Right Cessation
- 1970-06-03 NO NO2161/70A patent/NO125748B/no unknown
- 1970-06-04 JP JP45048661A patent/JPS4810360B1/ja active Pending
- 1970-06-04 DE DE2027371A patent/DE2027371C3/en not_active Expired
- 1970-06-05 BE BE751547D patent/BE751547A/en unknown
- 1970-06-05 GB GB2737770A patent/GB1311747A/en not_active Expired
- 1970-06-05 FR FR7020862A patent/FR2049166B1/fr not_active Expired

Also Published As

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

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Legal Events

Date	Code	Title	Description
1987-02-27	PL	Patent ceased