DE3760752D1 - Thrust regulating device for a solid-fuel propulsion unit - Google Patents

Thrust regulating device for a solid-fuel propulsion unit

Info

Publication number
DE3760752D1
DE3760752D1 DE8787400239T DE3760752T DE3760752D1 DE 3760752 D1 DE3760752 D1 DE 3760752D1 DE 8787400239 T DE8787400239 T DE 8787400239T DE 3760752 T DE3760752 T DE 3760752T DE 3760752 D1 DE3760752 D1 DE 3760752D1
Authority
DE
Germany
Prior art keywords
solid
regulating device
propulsion unit
fuel propulsion
thrust regulating
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
DE8787400239T
Other languages
English (en)
Inventor
Corre Alain Marie Le
Max Jean-Pierre Calabro
Gilles Bernard Vigier
Patrick Comtesse
Jean Francois Beau
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
Application granted granted Critical
Publication of DE3760752D1 publication Critical patent/DE3760752D1/de
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
    • F02K9/86—Rocket-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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lift Valve (AREA)
  • Portable Nailing Machines And Staplers (AREA)
DE8787400239T 1986-02-18 1987-02-03 Thrust regulating device for a solid-fuel propulsion unit Expired DE3760752D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8602148A FR2594490B1 (fr) 1986-02-18 1986-02-18 Dispositif pour faire varier la poussee d'un propulseur a propergol solide

Publications (1)

Publication Number Publication Date
DE3760752D1 true DE3760752D1 (en) 1989-11-16

Family

ID=9332219

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787400239T Expired DE3760752D1 (en) 1986-02-18 1987-02-03 Thrust regulating device for a solid-fuel propulsion unit

Country Status (4)

Country Link
US (1) US4777795A (de)
EP (1) EP0238369B1 (de)
DE (1) DE3760752D1 (de)
FR (1) FR2594490B1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5394690A (en) * 1993-09-20 1995-03-07 The United States Of America As Represented By The Secretary Of The Army Constant pressure, variable thrust bipropellant engine
US5435128A (en) * 1993-11-15 1995-07-25 Thiokol Corporation Pyrotechnically driven nozzle restrictor
US5491973A (en) * 1994-10-17 1996-02-20 Aerojet General Corporation Self-actuating control for rocket motor nozzle
FR2740106B1 (fr) * 1995-10-20 1998-01-09 Europ Propulsion Dispositif pour le pilotage d'engin spatial par vannage de gaz par tuyere mobile
US7849695B1 (en) * 2001-09-17 2010-12-14 Alliant Techsystems Inc. Rocket thruster comprising load-balanced pintle valve
US7565797B2 (en) * 2004-02-27 2009-07-28 Ghkn Engineering Llc Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles
US7509796B2 (en) * 2006-09-13 2009-03-31 Aerojet-General Corporation Pintle-controlled propulsion system with external dynamic seal
US20090211225A1 (en) * 2007-01-29 2009-08-27 Ghkn Engineering, Llc Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles
US20090260343A1 (en) * 2008-04-17 2009-10-22 Honeywell International Inc. Solid propellant management control system and method
US9677504B2 (en) 2010-05-11 2017-06-13 Orbital Atk, Inc. Rockets, methods of rocket control and methods of rocket evaluation utilizing pressure compensation
US9279503B2 (en) * 2011-06-20 2016-03-08 Streamline Automation, Llc Constant volume combustion chamber
CN103410632B (zh) * 2013-08-09 2015-06-17 南京理工大学 电动锥阀式固体火箭冲压发动机燃气流量调节装置
JP6129682B2 (ja) * 2013-08-12 2017-05-17 三菱重工業株式会社 推力制御バルブ及び飛翔体
EP3126661B1 (de) 2014-04-02 2020-02-19 AVIO S.p.A. Raketenmotor mit festtreibstoff
US11859579B1 (en) * 2019-07-29 2024-01-02 Triad National Security, Llc System for multiple burns from a rocket motor
ES2971133T3 (es) * 2020-09-21 2024-06-03 Roxel France Propulsor con conexión sometida a tensión térmicamente
CN113638823B (zh) * 2021-08-10 2022-06-17 北京理工大学 一种针阀式流量可调燃气发生器地面试验装置

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2552497A (en) * 1945-08-13 1951-05-08 Franklin E Roach Variable throat rocket nozzle
CH259489A (de) * 1946-06-01 1949-01-31 Dittli Alois Raketantriebsaggregat.
FR1128730A (fr) * 1955-07-09 1957-01-09 Soc Et Propulsion Par Reaction Moteur-fusée
NL246977A (de) * 1958-12-31
US3073112A (en) * 1959-09-21 1963-01-15 Olin Mathieson Rocket motor control system
US3069846A (en) * 1959-09-28 1962-12-25 Clary Corp Thrust device
FR1268781A (fr) * 1960-09-26 1961-08-04 Olin Mathieson Moteur de fusée et procédé de réglage de la poussée d'un moteur de fusée
US3349565A (en) * 1965-10-14 1967-10-31 Thiokol Chemical Corp Variable thrust solid propellant rocket motor
US3319423A (en) * 1966-05-24 1967-05-16 James M Caraher Water-cooled, self-regulating, exhaust nozzle for a submarine thermal power plant
US3948042A (en) * 1968-12-23 1976-04-06 The United States Of America As Represented By The Secretary Of The Navy System for controlling the nozzle throat area of a rocket motor
US3914935A (en) * 1969-03-17 1975-10-28 Rockwell International Corp Dual area nozzle
US3760589A (en) * 1969-03-24 1973-09-25 Thiokol Chemical Corp Throttling mechanism for controlling the thrust level of a solid propellant rocket motor
US3608312A (en) * 1969-10-22 1971-09-28 Us Navy Self-actuated dual area annular nozzle
FR2085297A1 (de) * 1970-04-07 1971-12-24 Europ Propulsion
US3726480A (en) * 1971-02-24 1973-04-10 Us Navy Thrust vectoring control system for rocket nozzles
US3943708A (en) * 1973-11-26 1976-03-16 The United States Of America As Represented By The Secretary Of The Navy Two area rocket nozzle

Also Published As

Publication number Publication date
FR2594490A1 (fr) 1987-08-21
US4777795A (en) 1988-10-18
FR2594490B1 (fr) 1989-09-15
EP0238369B1 (de) 1989-10-11
EP0238369A1 (de) 1987-09-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee