GB8506956D0 - Rockets & motors - Google Patents

Rockets & motors

Info

Publication number
GB8506956D0
GB8506956D0 GB858506956A GB8506956A GB8506956D0 GB 8506956 D0 GB8506956 D0 GB 8506956D0 GB 858506956 A GB858506956 A GB 858506956A GB 8506956 A GB8506956 A GB 8506956A GB 8506956 D0 GB8506956 D0 GB 8506956D0
Authority
GB
United Kingdom
Prior art keywords
rockets
motors
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.)
Granted
Application number
GB858506956A
Other versions
GB2156290B (en
GB2156290A (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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of GB8506956D0 publication Critical patent/GB8506956D0/en
Publication of GB2156290A publication Critical patent/GB2156290A/en
Application granted granted Critical
Publication of GB2156290B publication Critical patent/GB2156290B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/663Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/86Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles

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)
  • Testing Of Engines (AREA)
GB08506956A 1984-03-27 1985-03-18 Rockets and rocket motors Expired GB2156290B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8407919 1984-03-27

Publications (3)

Publication Number Publication Date
GB8506956D0 true GB8506956D0 (en) 1985-04-24
GB2156290A GB2156290A (en) 1985-10-09
GB2156290B GB2156290B (en) 1988-06-02

Family

ID=10558749

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08506956A Expired GB2156290B (en) 1984-03-27 1985-03-18 Rockets and rocket motors

Country Status (1)

Country Link
GB (1) GB2156290B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113687013A (en) * 2021-07-30 2021-11-23 西北工业大学 Device for shooting solid propellant combustion test under overload condition

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4760694A (en) * 1986-10-27 1988-08-02 Rockwell International Corporation Bi-level thruster
FR2655723B1 (en) * 1989-12-08 1993-01-22 Thomson Brandt Armements DEVICE FOR SEALING A NOZZLE FOR A GAS GENERATOR EQUIPPED WITH A FLYING MACHINE.
FR2784444B1 (en) * 1998-10-13 2000-12-29 Celerg METHOD AND DEVICE FOR CONTROLLING HOT GAS VALVE VALVES, PARTICULARLY FOR THE PILOTAGE AND / OR PROPULSION OF A MISSILE
US6591603B2 (en) * 2001-03-08 2003-07-15 Trw Inc. Pintle injector rocket with expansion-deflection nozzle
DE102004045855B4 (en) 2004-09-20 2006-06-29 Eads Space Transportation Gmbh Control and / or drive device for a missile
FR2970742B1 (en) 2011-01-20 2016-05-20 Mbda France DEVICE FOR CONTROLLING THE PASSAGE OF A GASEOUS JET IN A FLYING ENGINE TUYERE, AND FLYING ENGINE COMPRISING SUCH DEVICES
FR3002982B1 (en) * 2013-03-07 2015-04-10 Herakles GAS EJECTION SECTION MODULATION DEVICE.

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1488794A (en) * 1973-10-04 1977-10-12 Dresser Europe Sa Control valve
DE2424321A1 (en) * 1974-05-18 1975-11-20 Woma Maasberg Co Gmbh W SHUT-OFF VALVE FOR HIGH AND HIGHEST PRESSURES, IN PARTICULAR FOR HIGH PRESSURE GUNS
US4174824A (en) * 1977-05-13 1979-11-20 Eaton Corporation Pressure operated pilot control shut-off valve
ZA784019B (en) * 1978-07-14 1980-01-30 De Beers Ind Diamond Ejector valve assemblies
FR2504085A1 (en) * 1981-04-21 1982-10-22 Thomson Brandt DEVICE FOR STEAMING BY GAS JETS AND PROJECTILE COMPRISING SUCH A DEVICE
FR2508414B1 (en) * 1981-06-30 1985-06-07 Thomson Brandt GAS JET STEERING DEVICE FOR A GUIDED MACHINE
DE3144532A1 (en) * 1981-11-10 1983-05-19 Rheinmetall GmbH, 4000 Düsseldorf WING STABILIZED SHELL
FR2536720A1 (en) * 1982-11-29 1984-06-01 Aerospatiale SYSTEM FOR CONTROLLING A MISSILE USING LATERAL GAS JETS AND MISSILE HAVING SUCH A SYSTEM

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113687013A (en) * 2021-07-30 2021-11-23 西北工业大学 Device for shooting solid propellant combustion test under overload condition

Also Published As

Publication number Publication date
GB2156290B (en) 1988-06-02
GB2156290A (en) 1985-10-09

Similar Documents

Publication Publication Date Title
GB2154376B (en) External rotor motor
EP0180722A3 (en) Missile
GB2113811B (en) Rocket motors
IL76404A0 (en) Missile
GB8526803D0 (en) Stator
GB8526805D0 (en) Rotor
GB2162698B (en) Linear motors
CS339185A1 (en) Rotor elektrickeho stroje
GB8506956D0 (en) Rockets & motors
DE3565153D1 (en) Single stage autophage rocket
DE3479774D1 (en) Coreless-brushless motor
GB8505211D0 (en) Rotor
EP0162150A3 (en) Motor
GB8521927D0 (en) D c motor
GB2108641B (en) Rocket motors
GB2106988B (en) Rocket motors
GB8500298D0 (en) Rocket motors
GB2161029B (en) Motor
GB8324899D0 (en) Rocket motors
GB8524738D0 (en) Motor
GB8324900D0 (en) Rocket motors
CS406884A1 (en) Stator bareloveho radialniho turbokompresoru
CS464784A1 (en) Stator radialniho turbokompresoru
GB8526806D0 (en) Stator
GB8408100D0 (en) Improvements in rocket motors

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Effective date: 20050317