GB2005606B - Rocket propulsion unit for a guided missile - Google Patents

Rocket propulsion unit for a guided missile

Info

Publication number
GB2005606B
GB2005606B GB7839345A GB7839345A GB2005606B GB 2005606 B GB2005606 B GB 2005606B GB 7839345 A GB7839345 A GB 7839345A GB 7839345 A GB7839345 A GB 7839345A GB 2005606 B GB2005606 B GB 2005606B
Authority
GB
United Kingdom
Prior art keywords
propulsion unit
guided missile
rocket propulsion
rocket
missile
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
GB7839345A
Other versions
GB2005606A (en
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.)
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Original Assignee
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
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 Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH filed Critical Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Publication of GB2005606A publication Critical patent/GB2005606A/en
Application granted granted Critical
Publication of GB2005606B publication Critical patent/GB2005606B/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Nozzles (AREA)
GB7839345A 1977-10-06 1978-10-04 Rocket propulsion unit for a guided missile Expired GB2005606B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19772744897 DE2744897A1 (en) 1977-10-06 1977-10-06 STEERING BODY

Publications (2)

Publication Number Publication Date
GB2005606A GB2005606A (en) 1979-04-25
GB2005606B true GB2005606B (en) 1982-06-30

Family

ID=6020761

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7839345A Expired GB2005606B (en) 1977-10-06 1978-10-04 Rocket propulsion unit for a guided missile

Country Status (4)

Country Link
DE (1) DE2744897A1 (en)
FR (1) FR2405456A1 (en)
GB (1) GB2005606B (en)
IT (1) IT1099232B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2533637C2 (en) * 2010-07-22 2014-11-20 Сааб Аб Cooling device for cooling gaseous combustion products from recoilless anti-tank weapon
CN112572840A (en) * 2020-12-14 2021-03-30 兰州空间技术物理研究所 Electric propulsion system storage and supply unit and manufacturing method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147590A (en) * 1961-03-16 1964-09-08 Thompson Ramo Wooldridge Inc Reaction motor with nozzle vector control having ablative port means and cooled valve means
FR1316191A (en) * 1962-02-26 1963-01-25 United Aircraft Corp Control device for propellant
US3266732A (en) * 1963-09-03 1966-08-16 United Aircraft Corp Roll control system
US3270505A (en) * 1964-10-21 1966-09-06 Norman L Crabill Control system for rocket vehicles
GB1134835A (en) * 1965-12-06 1968-11-27 Us Navy Liquid injection thrust vectoring
US4063685A (en) * 1976-07-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle

Also Published As

Publication number Publication date
IT7828403A0 (en) 1978-10-04
GB2005606A (en) 1979-04-25
DE2744897A1 (en) 1979-04-19
IT1099232B (en) 1985-09-18
FR2405456A1 (en) 1979-05-04

Similar Documents

Publication Publication Date Title
NZ187168A (en) Self propelled unmanned submarine
AU514128B2 (en) Steering arrangement for projectiles ofthe missile kind
JPS5646999A (en) Missile
IL54132A (en) Thrust direction reverser for jet engine
JPS568795A (en) Propelling device for ships
GB2039619B (en) Rocket propulsion system
IL55473A (en) Sub-calibre arrow-shaped missile having a resistance-stabilising rear part
JPS5459516A (en) Liquid rocket propulsion device
GB2100847B (en) Device for launching a projectile
GB2078912B (en) Missile launcher
GB2006936A (en) Finstabilised practice missile
GB2002093B (en) Percussion-fuse for missiles
GB2005606B (en) Rocket propulsion unit for a guided missile
JPS52123600A (en) Missile safety mechanism
GB2007773B (en) Nozzle for propulsion units
GB1542243A (en) Assembly for launching a projectile
IT1193489B (en) FRONT PROPULSION VESSEL
GB2011589B (en) Propulsion unit and process for the acceleration of a missile
GB2162926B (en) A solid rocket propulsion system
DE3061241D1 (en) Thrust vector control for a solid-propellant rocket
GB2162927B (en) A solid rocket propulsion system
JPS5656597A (en) Rocket launching system
GB2012881B (en) Jet propulsion efflux outlets
JPS5388311A (en) Composite type propellant
GB2061471B (en) Means for initially stabilizing a rocket

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)
PCNP Patent ceased through non-payment of renewal fee