IT9067979A0 - DEVICE FOR CLOSING A NOZZLE FOR A GAS GENERATOR EQUIPPING A FLYING ORDN - Google Patents

DEVICE FOR CLOSING A NOZZLE FOR A GAS GENERATOR EQUIPPING A FLYING ORDN

Info

Publication number
IT9067979A0
IT9067979A0 IT67979A IT6797990A IT9067979A0 IT 9067979 A0 IT9067979 A0 IT 9067979A0 IT 67979 A IT67979 A IT 67979A IT 6797990 A IT6797990 A IT 6797990A IT 9067979 A0 IT9067979 A0 IT 9067979A0
Authority
IT
Italy
Prior art keywords
ordn
flying
nozzle
closing
gas generator
Prior art date
Application number
IT67979A
Other languages
Italian (it)
Other versions
IT1241020B (en
IT9067979A1 (en
Inventor
Marc Bernard
Rene Thouron
Original Assignee
Thomson Brandt Armements
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 Thomson Brandt Armements filed Critical Thomson Brandt Armements
Publication of IT9067979A0 publication Critical patent/IT9067979A0/en
Publication of IT9067979A1 publication Critical patent/IT9067979A1/en
Application granted granted Critical
Publication of IT1241020B publication Critical patent/IT1241020B/en

Links

Classifications

    • 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
    • F02K9/74Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Plasma Technology (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Slot Machines And Peripheral Devices (AREA)
  • Devices For Medical Bathing And Washing (AREA)
  • Portable Nailing Machines And Staplers (AREA)
IT67979A 1989-12-08 1990-12-07 NOZZLE CLOSING DEVICE FOR A GAS GENERATOR PROVIDED WITH A FLYING ORDER IT1241020B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8916263A FR2655723B1 (en) 1989-12-08 1989-12-08 DEVICE FOR SEALING A NOZZLE FOR A GAS GENERATOR EQUIPPED WITH A FLYING MACHINE.

Publications (3)

Publication Number Publication Date
IT9067979A0 true IT9067979A0 (en) 1990-12-07
IT9067979A1 IT9067979A1 (en) 1991-06-09
IT1241020B IT1241020B (en) 1993-12-27

Family

ID=9388298

Family Applications (1)

Application Number Title Priority Date Filing Date
IT67979A IT1241020B (en) 1989-12-08 1990-12-07 NOZZLE CLOSING DEVICE FOR A GAS GENERATOR PROVIDED WITH A FLYING ORDER

Country Status (3)

Country Link
FR (1) FR2655723B1 (en)
GB (1) GB2238857A (en)
IT (1) IT1241020B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5435128A (en) * 1993-11-15 1995-07-25 Thiokol Corporation Pyrotechnically driven nozzle restrictor
RU2461729C1 (en) * 2011-08-02 2012-09-20 Николай Евгеньевич Староверов Self-adjusted two-mode nozzle (versions)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2613497A (en) * 1947-04-01 1952-10-14 Macdonald Gilmour Craig Controllable rocket thrust device
US3230704A (en) * 1961-10-30 1966-01-25 Thiokol Chemical Corp Rocket engine
US3329089A (en) * 1964-12-24 1967-07-04 Herbert L Harrison Retention-release mechanism for reaction motors and rocket interstages
US3691770A (en) * 1966-12-02 1972-09-19 Us Navy Thrust control means for a solid propellant rocket motor
GB1538192A (en) * 1968-05-18 1979-01-10 Karlsruhe Augsburg Iweka Cartridge-type missile
DE2320076A1 (en) * 1973-04-19 1974-11-14 Norbert Mieseler ADJUSTABLE ROCKET MOTOR
DE2605428A1 (en) * 1976-02-12 1977-08-18 Messerschmitt Boelkow Blohm COMPRESSED GAS TANK FOR ONE FLOOR
SE419800B (en) * 1978-02-23 1981-08-24 Sven Landstrom REMSPROJEKTIL
GB2156290B (en) * 1984-03-27 1988-06-02 British Aerospace Rockets and rocket motors

Also Published As

Publication number Publication date
FR2655723B1 (en) 1993-01-22
GB2238857A (en) 1991-06-12
IT1241020B (en) 1993-12-27
FR2655723A1 (en) 1991-06-14
GB9026535D0 (en) 1991-01-23
IT9067979A1 (en) 1991-06-09

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Legal Events

Date Code Title Description
0001 Granted