NO985004D0 - Tverrskyv-styreanordning for flylegemer med faststoff-gassgenerator - Google Patents

Tverrskyv-styreanordning for flylegemer med faststoff-gassgenerator

Info

Publication number
NO985004D0
NO985004D0 NO985004A NO985004A NO985004D0 NO 985004 D0 NO985004 D0 NO 985004D0 NO 985004 A NO985004 A NO 985004A NO 985004 A NO985004 A NO 985004A NO 985004 D0 NO985004 D0 NO 985004D0
Authority
NO
Norway
Prior art keywords
solid
control device
gas generator
transverse sliding
sliding control
Prior art date
Application number
NO985004A
Other languages
English (en)
Other versions
NO311454B1 (no
NO985004L (no
Inventor
Karl Smirra
Original Assignee
Lfk Lenkflugk Rpersysteme Gmbh
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
Priority to DE19735279A priority Critical patent/DE19735279C1/de
Priority to FR9809785A priority patent/FR2767382B1/fr
Priority to IT1998MI001868A priority patent/IT1302150B1/it
Application filed by Lfk Lenkflugk Rpersysteme Gmbh filed Critical Lfk Lenkflugk Rpersysteme Gmbh
Priority to NO19985004A priority patent/NO311454B1/no
Publication of NO985004D0 publication Critical patent/NO985004D0/no
Priority to GB9824042A priority patent/GB2343424B/en
Publication of NO985004L publication Critical patent/NO985004L/no
Publication of NO311454B1 publication Critical patent/NO311454B1/no

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
    • F02K9/80Rocket-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
    • F02K9/805Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Air Bags (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Tents Or Canopies (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Mechanically-Actuated Valves (AREA)
NO19985004A 1997-08-14 1998-10-27 Tverrskyv-styreanordning for flylegemer med faststoff- gassgenerator NO311454B1 (no)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE19735279A DE19735279C1 (de) 1997-08-14 1997-08-14 Querschub-Steueranordnung für Flugkörper mit Feststoff-Heißgasgenerator
FR9809785A FR2767382B1 (fr) 1997-08-14 1998-07-30 Dispositif de commande de poussee transversale pour missiles, comportant un generateur de gaz chauds a matiere solide
IT1998MI001868A IT1302150B1 (it) 1997-08-14 1998-08-07 Disposizione di comando di getti trasversali per aerodina congeneratore di gas caldo a propellente solido.
NO19985004A NO311454B1 (no) 1997-08-14 1998-10-27 Tverrskyv-styreanordning for flylegemer med faststoff- gassgenerator
GB9824042A GB2343424B (en) 1997-08-14 1998-11-03 Transverse thrust control arrangement for missiles

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19735279A DE19735279C1 (de) 1997-08-14 1997-08-14 Querschub-Steueranordnung für Flugkörper mit Feststoff-Heißgasgenerator
NO19985004A NO311454B1 (no) 1997-08-14 1998-10-27 Tverrskyv-styreanordning for flylegemer med faststoff- gassgenerator
GB9824042A GB2343424B (en) 1997-08-14 1998-11-03 Transverse thrust control arrangement for missiles

Publications (3)

Publication Number Publication Date
NO985004D0 true NO985004D0 (no) 1998-10-27
NO985004L NO985004L (no) 2000-04-28
NO311454B1 NO311454B1 (no) 2001-11-26

Family

ID=27217648

Family Applications (1)

Application Number Title Priority Date Filing Date
NO19985004A NO311454B1 (no) 1997-08-14 1998-10-27 Tverrskyv-styreanordning for flylegemer med faststoff- gassgenerator

Country Status (5)

Country Link
DE (1) DE19735279C1 (no)
FR (1) FR2767382B1 (no)
GB (1) GB2343424B (no)
IT (1) IT1302150B1 (no)
NO (1) NO311454B1 (no)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102582827A (zh) * 2012-02-11 2012-07-18 黄廷华 一种能任意移动的飞行装置
CN107314716B (zh) * 2017-07-13 2019-02-12 乐清市拓展机械科技有限公司 一种跟踪发射体
DE102017129941A1 (de) 2017-12-14 2019-06-19 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Ventil für ein regelbares Querschubtriebwerk
DE102017130117A1 (de) 2017-12-15 2019-06-19 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Um eine Achse drehbarer Ventilkörper für ein regelbares Querschubtriebwerk

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4017040A (en) * 1976-01-12 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Steerable extraction rocket
FR2504085A1 (fr) * 1981-04-21 1982-10-22 Thomson Brandt Dispositif de pilotage par jets de gaz et projectile comprenant un tel dispositif
DE3519892A1 (de) * 1985-06-04 1986-12-04 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Brems- und freigabeeinrichtung fuer einen drehduesenkoerper
DE3537079C1 (en) * 1985-10-18 1987-02-19 Messerschmitt Boelkow Blohm Quick-acting fluid control valve esp. for supersonic aircraft - has piston actuated by gas to deflect retaining balls
FR2620812B1 (fr) * 1987-09-18 1992-04-17 Thomson Brandt Armements Dispositif de commutation de jets de gaz lateraux destine au pilotage d'engins
DE3901041A1 (de) * 1989-01-14 1990-07-26 Messerschmitt Boelkow Blohm Lenkgeschoss
FR2659734B1 (fr) * 1990-03-14 1992-07-03 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux.
FR2730302B1 (fr) * 1995-02-03 1997-03-14 Tda Armements Sas Controle d'un projectile par impulseur multi-chambre et mono-tuyere
US5711348A (en) * 1996-08-14 1998-01-27 Moog Inc. Hot gas control valve

Also Published As

Publication number Publication date
ITMI981868A1 (it) 2000-02-07
FR2767382B1 (fr) 2003-10-03
ITMI981868A0 (it) 1998-08-07
GB2343424B (en) 2001-06-13
IT1302150B1 (it) 2000-07-31
NO311454B1 (no) 2001-11-26
FR2767382A1 (fr) 1999-02-19
DE19735279C1 (de) 1999-03-11
GB9824042D0 (en) 1998-12-30
NO985004L (no) 2000-04-28
GB2343424A (en) 2000-05-10

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Legal Events

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