DE3669564D1 - Hydraulisches antriebsystem fuer ein teil in einer rakete. - Google Patents

Hydraulisches antriebsystem fuer ein teil in einer rakete.

Info

Publication number
DE3669564D1
DE3669564D1 DE8686400689T DE3669564T DE3669564D1 DE 3669564 D1 DE3669564 D1 DE 3669564D1 DE 8686400689 T DE8686400689 T DE 8686400689T DE 3669564 T DE3669564 T DE 3669564T DE 3669564 D1 DE3669564 D1 DE 3669564D1
Authority
DE
Germany
Prior art keywords
rocket
drive system
hydraulic drive
hydraulic
drive
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 - Fee Related
Application number
DE8686400689T
Other languages
English (en)
Inventor
Francois Paris
Claude Johnson
Albert Lecrivain
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Application granted granted Critical
Publication of DE3669564D1 publication Critical patent/DE3669564D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G5/00—Ground equipment for vehicles, e.g. starting towers, fuelling arrangements
    • 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
    • F02K9/805—Rocket-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
    • 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
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Remote Sensing (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
DE8686400689T 1985-04-04 1986-03-28 Hydraulisches antriebsystem fuer ein teil in einer rakete. Expired - Fee Related DE3669564D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8505144A FR2580038B1 (de) 1985-04-04 1985-04-04

Publications (1)

Publication Number Publication Date
DE3669564D1 true DE3669564D1 (de) 1990-04-19

Family

ID=9317950

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686400689T Expired - Fee Related DE3669564D1 (de) 1985-04-04 1986-03-28 Hydraulisches antriebsystem fuer ein teil in einer rakete.

Country Status (4)

Country Link
US (1) US4757960A (de)
EP (1) EP0201374B1 (de)
DE (1) DE3669564D1 (de)
FR (1) FR2580038B1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6070408A (en) * 1997-11-25 2000-06-06 Caterpillar Inc. Hydraulic apparatus with improved accumulator for reduced pressure pulsation and method of operating the same
US6802406B2 (en) * 2002-12-17 2004-10-12 United Defense, L.P. Recoil brake isolation system
US7687930B2 (en) * 2007-09-10 2010-03-30 Hansen Jr Howard Otto Solar/geothermal powered thermodynamic hydro electric generating system
US7579700B1 (en) * 2008-05-28 2009-08-25 Moshe Meller System and method for converting electrical energy into pressurized air and converting pressurized air into electricity
CN107867411B (zh) * 2017-09-20 2021-02-09 上海空间推进研究所 一种全自动在轨补加装置
CN108045604B (zh) * 2017-12-07 2020-11-24 上海宇航系统工程研究所 一种连接器气动随动装置

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2170890A (en) * 1937-04-08 1939-08-29 Link Belt Co Removable accumulator
US2278181A (en) * 1939-05-17 1942-03-31 Sulzer Ag Engine and gear coupling
US2290479A (en) * 1939-06-02 1942-07-21 Mercier Jean Hydraulic control system
US2866385A (en) * 1956-01-10 1958-12-30 Northrop Aircraft Inc Automatic jet engine starting device
US3049877A (en) * 1956-02-13 1962-08-21 Thiokol Chemical Corp Nozzle for reaction motor
US3908933A (en) * 1956-06-26 1975-09-30 Us Navy Guided missile
FR1237219A (fr) * 1959-06-16 1960-07-29 France Etat Tuyère orientable
US3163985A (en) * 1962-07-31 1965-01-05 John V Bouyoucos Hydraulic energy storage system
FR1469194A (fr) * 1965-12-30 1967-02-10 Onera (Off Nat Aerospatiale) Perfectionnements apportés aux missiles à générateur de gaz à au moins un ergolliquide soumis à la pression directe d'un gaz de chasse et aux installations de lancement de tels missiles
GB1250491A (de) * 1967-12-15 1971-10-20
US3692258A (en) * 1968-10-03 1972-09-19 Arthur R Parilla Missile configurations,controls and utilization techniques
GB1291586A (en) * 1969-10-23 1972-10-04 Rolls Royce Propulsive jet nozzle assembly
US3911678A (en) * 1974-11-07 1975-10-14 Shafer Valve Co Safety shut-off for pump
FR2444805A1 (fr) * 1978-12-20 1980-07-18 Europ Propulsion Dispositif de deviation du jet d'une tuyere de propulseur-fusee

Also Published As

Publication number Publication date
US4757960A (en) 1988-07-19
FR2580038B1 (de) 1987-06-19
EP0201374A1 (de) 1986-11-12
FR2580038A1 (de) 1986-10-10
EP0201374B1 (de) 1990-03-14

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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