FR2049166A1 - - Google Patents

Info

Publication number
FR2049166A1
FR2049166A1 FR7020862A FR7020862A FR2049166A1 FR 2049166 A1 FR2049166 A1 FR 2049166A1 FR 7020862 A FR7020862 A FR 7020862A FR 7020862 A FR7020862 A FR 7020862A FR 2049166 A1 FR2049166 A1 FR 2049166A1
Authority
FR
France
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
FR7020862A
Other languages
French (fr)
Other versions
FR2049166B1 (de
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 FR2049166A1 publication Critical patent/FR2049166A1/fr
Application granted granted Critical
Publication of FR2049166B1 publication Critical patent/FR2049166B1/fr
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)
FR7020862A 1969-06-06 1970-06-05 Expired FR2049166B1 (de)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2049166A1 true FR2049166A1 (de) 1971-03-26
FR2049166B1 FR2049166B1 (de) 1974-05-24

Family

ID=20273043

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7020862A Expired FR2049166B1 (de) 1969-06-06 1970-06-05

Country Status (10)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463909A1 (fr) * 1979-08-17 1981-02-27 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2500149A1 (fr) * 1981-02-17 1982-08-20 Poudres & Explosifs Ste Nale Chargement propulsif biregime a canal en trompette comportant une section en etoile

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172383B (en) * 1981-06-04 1987-08-12 Aerospatiale Guided missile system
FR2578665B1 (fr) * 1981-06-04 1988-02-12 Aerospatiale Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede
FR2863665B1 (fr) * 1988-10-12 2007-03-30 Aerospatiale Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur
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 (zh) * 2018-01-12 2019-05-24 北京航空航天大学 一种便于调整的模块化配重装置及火箭

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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463909A1 (fr) * 1979-08-17 1981-02-27 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
EP0025373A1 (de) * 1979-08-17 1981-03-18 Thomson-Brandt Verfahren zum Leiten oder Führen eines Flugkörpers und mit Mitteln zur Durchführung dieses Verfahrens ausgerüsteter Flugkörper
FR2500149A1 (fr) * 1981-02-17 1982-08-20 Poudres & Explosifs Ste Nale Chargement propulsif biregime a canal en trompette comportant une section en etoile
EP0059142A1 (de) * 1981-02-17 1982-09-01 Societe Nationale Des Poudres Et Explosifs Feststofftreibsatz für zwei Schubbereiche mit einem Zentralkanal und einem Sternbrennerabschnitt

Also Published As

Publication number Publication date
NL161255B (nl) 1979-08-15
DE2027371B2 (de) 1979-05-03
SE340417B (de) 1971-11-15
NL7007998A (de) 1970-12-08
NL161255C (nl) 1980-01-15
NO125748B (de) 1972-10-23
US3684215A (en) 1972-08-15
CH508863A (de) 1971-06-15
GB1311747A (en) 1973-03-28
FR2049166B1 (de) 1974-05-24
DE2027371C3 (de) 1980-01-03
JPS4810360B1 (de) 1973-04-02
DE2027371A1 (de) 1970-12-10
BE751547A (fr) 1970-11-16

Similar Documents

Publication Publication Date Title
AU465452B2 (de)
CS153060B2 (de)
AU429630B2 (de)
AU450150B2 (de)
FR2049166B1 (de)
AU442375B2 (de)
AU470301B1 (de)
AU442357B2 (de)
AU442285B2 (de)
AU438128B2 (de)
AU442322B2 (de)
AU414607B2 (de)
AU442554B2 (de)
AU442380B2 (de)
AU442463B2 (de)
AU442535B2 (de)
AU470661B1 (de)
AU442538B2 (de)
CS153039B2 (de)
CS148487B1 (de)
CS150368B1 (de)
AU5109569A (de)
BE742135A (de)
AU469091A (de)
CH574925A5 (de)

Legal Events

Date Code Title Description
ST Notification of lapse