FR2450356B1 - - Google Patents

Info

Publication number
FR2450356B1
FR2450356B1 FR7904987A FR7904987A FR2450356B1 FR 2450356 B1 FR2450356 B1 FR 2450356B1 FR 7904987 A FR7904987 A FR 7904987A FR 7904987 A FR7904987 A FR 7904987A FR 2450356 B1 FR2450356 B1 FR 2450356B1
Authority
FR
France
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
FR7904987A
Other languages
French (fr)
Other versions
FR2450356A1 (fr
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7904987A priority Critical patent/FR2450356A1/fr
Priority to US06/124,349 priority patent/US4424670A/en
Priority to EP80400263A priority patent/EP0015216B1/fr
Priority to DE8080400263T priority patent/DE3061241D1/de
Publication of FR2450356A1 publication Critical patent/FR2450356A1/fr
Application granted granted Critical
Publication of FR2450356B1 publication Critical patent/FR2450356B1/fr
Granted 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
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Nozzles (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Steering Controls (AREA)
FR7904987A 1979-02-27 1979-02-27 Agencement de pilotage d'un propulseur d'engin a propergol solide Granted FR2450356A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7904987A FR2450356A1 (fr) 1979-02-27 1979-02-27 Agencement de pilotage d'un propulseur d'engin a propergol solide
US06/124,349 US4424670A (en) 1979-02-27 1980-02-25 Device for piloting the propulsion system of a solid propellant rocket
EP80400263A EP0015216B1 (fr) 1979-02-27 1980-02-26 Agencement de pilotage d'un propulseur d'engin à propergol solide
DE8080400263T DE3061241D1 (en) 1979-02-27 1980-02-26 Thrust vector control for a solid-propellant rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7904987A FR2450356A1 (fr) 1979-02-27 1979-02-27 Agencement de pilotage d'un propulseur d'engin a propergol solide

Publications (2)

Publication Number Publication Date
FR2450356A1 FR2450356A1 (fr) 1980-09-26
FR2450356B1 true FR2450356B1 (US06653308-20031125-C00199.png) 1983-02-18

Family

ID=9222493

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7904987A Granted FR2450356A1 (fr) 1979-02-27 1979-02-27 Agencement de pilotage d'un propulseur d'engin a propergol solide

Country Status (4)

Country Link
US (1) US4424670A (US06653308-20031125-C00199.png)
EP (1) EP0015216B1 (US06653308-20031125-C00199.png)
DE (1) DE3061241D1 (US06653308-20031125-C00199.png)
FR (1) FR2450356A1 (US06653308-20031125-C00199.png)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4484439A (en) * 1981-07-20 1984-11-27 Thiokol Corporation Thrust reversal system
FR2632722B1 (fr) * 1988-06-10 1993-09-03 Thomson Brandt Armements Dispositif destine a modifier la trajectoire d'un projectile par impulseurs pyrotechniques
ATE243809T1 (de) 1999-02-16 2003-07-15 Alliant Techsystems Inc Feststoffbrennsatzanordnung zur erzeugung einer gegen den verschleiss an einer raketendüse schützenden grenzschichtströmung
US6951317B2 (en) * 2002-09-03 2005-10-04 Honeywell International Inc. Vehicle, lightweight pneumatic pilot valve and related systems therefor

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3091924A (en) * 1960-12-15 1963-06-04 United Aircraft Corp Gaseous nozzle boundary
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
US3195303A (en) * 1962-01-22 1965-07-20 Bendix Corp Vortex valve
US3296799A (en) * 1965-08-27 1967-01-10 Thiokol Chemical Corp Thrust vector control system
US3370794A (en) * 1965-11-08 1968-02-27 Navy Usa Annular plenum nozzle for controlling trajectory of rockets
FR1488319A (fr) * 1966-04-28 1967-07-13 Snecma Perfectionnements au guidage des engins, notamment des engins ayant une tuyère propulsive à corps central
FR1522555A (fr) * 1967-03-17 1968-04-26 Snecma Dispositif de gouverne par déviation de jet
US3759039A (en) * 1968-11-22 1973-09-18 Thiokol Chemical Corp Thrust control and modulation system
FR2038073A1 (US06653308-20031125-C00199.png) * 1969-03-27 1971-01-08 Caumartin Yves
GB1434195A (en) * 1972-08-01 1976-05-05 Secr Defence Rocket motor thrust vector control means
FR2408037A1 (fr) * 1977-11-07 1979-06-01 Aerospatiale Tuyere chaude

Also Published As

Publication number Publication date
EP0015216B1 (fr) 1982-12-08
FR2450356A1 (fr) 1980-09-26
DE3061241D1 (en) 1983-01-13
EP0015216A1 (fr) 1980-09-03
US4424670A (en) 1984-01-10

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Legal Events

Date Code Title Description
ST Notification of lapse