SE340417B - - Google Patents

Info

Publication number
SE340417B
SE340417B SE08063/69A SE806369A SE340417B SE 340417 B SE340417 B SE 340417B SE 08063/69 A SE08063/69 A SE 08063/69A SE 806369 A SE806369 A SE 806369A SE 340417 B SE340417 B SE 340417B
Authority
SE
Sweden
Prior art keywords
missile
fuel
fuel charges
jet nozzles
propulsion motor
Prior art date
Application number
SE08063/69A
Other languages
English (en)
Inventor
G Jacobson
O Olsson
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
Priority to SE08063/69A priority Critical patent/SE340417B/xx
Priority to US41373A priority patent/US3684215A/en
Priority to NL7007998.A priority patent/NL161255C/xx
Priority to NO2161/70A priority patent/NO125748B/no
Priority to CH832570A priority patent/CH508863A/de
Priority to JP45048661A priority patent/JPS4810360B1/ja
Priority to DE2027371A priority patent/DE2027371C3/de
Priority to GB2737770A priority patent/GB1311747A/en
Priority to BE751547D priority patent/BE751547A/xx
Priority to FR7020862A priority patent/FR2049166B1/fr
Publication of SE340417B publication Critical patent/SE340417B/xx

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)
SE08063/69A 1969-06-06 1969-06-06 SE340417B (enrdf_load_stackoverflow)

Priority Applications (10)

Application Number Priority Date Filing Date Title
SE08063/69A SE340417B (enrdf_load_stackoverflow) 1969-06-06 1969-06-06
US41373A US3684215A (en) 1969-06-06 1970-05-28 Missile
NL7007998.A NL161255C (nl) 1969-06-06 1970-06-02 Projectiel.
NO2161/70A NO125748B (enrdf_load_stackoverflow) 1969-06-06 1970-06-03
CH832570A CH508863A (de) 1969-06-06 1970-06-03 Flugkörper mit Stabilisierungsflügeln und Festkörper-Antriebsvorrichtung
JP45048661A JPS4810360B1 (enrdf_load_stackoverflow) 1969-06-06 1970-06-04
DE2027371A DE2027371C3 (de) 1969-06-06 1970-06-04 Flugkörper mit Stabilisierungsflügeln und einem Festreibstoff-Triebwerk mit zwei gesonderten Treibsätzen
GB2737770A GB1311747A (en) 1969-06-06 1970-06-05 Missile
BE751547D BE751547A (fr) 1969-06-06 1970-06-05 Missile guide
FR7020862A FR2049166B1 (enrdf_load_stackoverflow) 1969-06-06 1970-06-05

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
SE340417B true SE340417B (enrdf_load_stackoverflow) 1971-11-15

Family

ID=20273043

Family Applications (1)

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

Country Status (10)

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

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463909B1 (fr) * 1979-08-17 1985-10-25 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2500149B1 (fr) * 1981-02-17 1985-12-06 Poudres & Explosifs Ste Nale Chargement propulsif biregime a canal en trompette comportant une section en etoile
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
GB2172383B (en) * 1981-06-04 1987-08-12 Aerospatiale Guided missile system
USH159H (en) 1984-12-17 1986-11-04 The United States Of America As Represented By The Secretary Of The Navy Shaped trajectory cruise missile launch mode
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
RU2135944C1 (ru) * 1998-08-10 1999-08-27 ГУП "Конструкторское бюро приборостроения" Управляемая ракета
RU2166724C1 (ru) * 2000-04-03 2001-05-10 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Управляемый снаряд
RU2258896C1 (ru) * 2004-05-05 2005-08-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Управляемая ракета в контейнере
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

Also Published As

Publication number Publication date
DE2027371C3 (de) 1980-01-03
JPS4810360B1 (enrdf_load_stackoverflow) 1973-04-02
NL161255B (nl) 1979-08-15
NL161255C (nl) 1980-01-15
DE2027371A1 (de) 1970-12-10
NO125748B (enrdf_load_stackoverflow) 1972-10-23
NL7007998A (enrdf_load_stackoverflow) 1970-12-08
FR2049166A1 (enrdf_load_stackoverflow) 1971-03-26
GB1311747A (en) 1973-03-28
US3684215A (en) 1972-08-15
CH508863A (de) 1971-06-15
BE751547A (fr) 1970-11-16
DE2027371B2 (de) 1979-05-03
FR2049166B1 (enrdf_load_stackoverflow) 1974-05-24

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