IT1237899B - SPACE VEHICLE WITH INCREASED FUEL LOAD TO CONTROL ITS ORIENTATION - Google Patents

SPACE VEHICLE WITH INCREASED FUEL LOAD TO CONTROL ITS ORIENTATION

Info

Publication number
IT1237899B
IT1237899B IT02268889A IT2268889A IT1237899B IT 1237899 B IT1237899 B IT 1237899B IT 02268889 A IT02268889 A IT 02268889A IT 2268889 A IT2268889 A IT 2268889A IT 1237899 B IT1237899 B IT 1237899B
Authority
IT
Italy
Prior art keywords
orientation
control
space vehicle
increased fuel
fuel load
Prior art date
Application number
IT02268889A
Other languages
Italian (it)
Other versions
IT8922688A0 (en
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8922688A0 publication Critical patent/IT8922688A0/en
Application granted granted Critical
Publication of IT1237899B publication Critical patent/IT1237899B/en

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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • 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
    • B64G1/242—Orbits and trajectories
    • 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
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Testing Of Engines (AREA)
  • Liquid Carbonaceous Fuels (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT02268889A 1988-12-16 1989-12-14 SPACE VEHICLE WITH INCREASED FUEL LOAD TO CONTROL ITS ORIENTATION IT1237899B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/285,699 US5263666A (en) 1988-12-16 1988-12-16 Spacecraft with increased stationkeeping fuel load

Publications (2)

Publication Number Publication Date
IT8922688A0 IT8922688A0 (en) 1989-12-14
IT1237899B true IT1237899B (en) 1993-06-18

Family

ID=23095359

Family Applications (1)

Application Number Title Priority Date Filing Date
IT02268889A IT1237899B (en) 1988-12-16 1989-12-14 SPACE VEHICLE WITH INCREASED FUEL LOAD TO CONTROL ITS ORIENTATION

Country Status (7)

Country Link
US (1) US5263666A (en)
JP (1) JPH02212299A (en)
CA (1) CA1331596C (en)
DE (1) DE3939910C2 (en)
FR (1) FR2640579B1 (en)
GB (1) GB2226999B (en)
IT (1) IT1237899B (en)

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DE69100603T2 (en) * 1990-02-26 1994-03-10 Aerospatiale Geostationary observation satellite with a multi-nozzle liquid fuel-driven apogee maneuvering system.
FR2667299B1 (en) * 1990-10-02 1994-01-14 Aerospatiale Ste Nationale Indle GEOSTATIONARY-TYPE SATELLITE WITH HANDLING SYSTEM HAVING LIQUID ERGOLS AND HOLLOW ANTENNAS.
US5169094A (en) * 1990-02-26 1992-12-08 Aerospatiale Societe Nationale Industrielle Geostationary earth observation satellite incorporating liquid propellant apogee maneuver system and hollow antennas
FR2664562B1 (en) * 1990-07-13 1996-03-08 Aerospatiale GEOSTATIONARY-TYPE SATELLITE HAVING A HANDLING SYSTEM HAVING A COMBINATION WITH LIQUID ERGOLS AND MULTIPLE TUYERES.
US5417049A (en) * 1990-04-19 1995-05-23 Trw Inc. Satellite propulsion and power system
US5282357A (en) * 1990-04-19 1994-02-01 Trw Inc. High-performance dual-mode integral propulsion system
US5251852A (en) * 1991-09-06 1993-10-12 General Electric Company Thermal fuel transfer and tank isolation to reduce unusable fuel
GB9127433D0 (en) * 1991-12-27 1992-02-19 Matra Marconi Space Uk Propulsion system for spacecraft
US5395076A (en) * 1993-03-19 1995-03-07 Martin Marietta Corporation Spacecraft velocity change maneuvers by variable arcjets
US5499656A (en) * 1993-12-23 1996-03-19 Hughes Aircraft Company Integrated storage and transfer system and method for spacecraft propulsion systems
US5816539A (en) * 1994-02-18 1998-10-06 Lockheed Martin Corporation Orbital assist module and interstage
US5651515A (en) * 1995-01-30 1997-07-29 Agence Spatiale Europeenne Method for re-orbiting a dual-mode propulsion geostationary spacecraft
FR2730831B1 (en) * 1995-02-22 1997-06-13 Centre Nat Etd Spatiales PRESSURIZATION DEVICE OF A UNIFIED LIQUID PROPULSION SUBSYSTEM OF A GEOSTATIONARY SATELLITE
US5823478A (en) * 1995-07-17 1998-10-20 The University Of British Columbia Pressure feed for liquid propellant
US5826830A (en) * 1995-12-22 1998-10-27 Hughes Electronics Corporation Dual-half system, full torque reaction control thruster configuration for three-axis stabilized spacecraft
US6024328A (en) * 1996-12-18 2000-02-15 Hughes Electronics Corporation Satellite control method using single species of bipropellant
FR2757824B1 (en) * 1996-12-31 1999-03-26 Europ Propulsion METHOD AND SYSTEM FOR LAUNCHING SATELLITES ON NON-COPLANAR ORBITS USING LUNAR GRAVITATIONAL ASSISTANCE
US5924648A (en) * 1997-10-03 1999-07-20 Lockheed Martin Corporation System for upending/reclining launch vehicles
US6135393A (en) * 1997-11-25 2000-10-24 Trw Inc. Spacecraft attitude and velocity control thruster system
US6341762B1 (en) * 1999-05-18 2002-01-29 Lockheed Martin Corporation Service valve and use of same in reaction control system
US6439507B1 (en) * 2000-05-05 2002-08-27 Space Systems/Loral, Inc. Closed-loop spacecraft orbit control
US6631314B2 (en) * 2001-05-22 2003-10-07 Lockheed Martin Corporation Propellant utilization system
US6739555B2 (en) * 2001-08-03 2004-05-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reusable module for the storage, transportation, and supply of multiple propellants in a space environment
US6726154B2 (en) * 2001-11-30 2004-04-27 United Technologies Corporation Reusable space access launch vehicle system
US7051980B2 (en) * 2002-02-26 2006-05-30 Lockheed Martin Corporation Efficient orbit sparing system for space vehicle constellations
US6672542B2 (en) * 2002-06-03 2004-01-06 The Aerospace Corporation Method and system for controlling the eccentricity of a near-circular orbit
US7477966B1 (en) 2004-02-20 2009-01-13 Lockheed Martin Corporation Propellant management system and method for multiple booster rockets
FR2878505B1 (en) * 2004-11-26 2007-01-12 Eads Space Transp Sa Sa ASSEMBLY FOR PROPULSION SYSTEM OF SPACE ENGINE AND PROPULSION SYSTEM COMPRISING AT LEAST ONE SUCH ASSEMBLY
US7762498B1 (en) * 2005-06-09 2010-07-27 Lockheed Martin Corporation Enhanced high-efficiency spacecraft propulsion system
US7454272B1 (en) * 2005-08-25 2008-11-18 Raytheon Company Geostationary stationkeeping method
DE102007043684B4 (en) * 2007-08-21 2010-05-12 Mt Aerospace Ag Method for filling tanks of aerospace missiles
WO2010036291A2 (en) * 2008-06-20 2010-04-01 Aerojet-General Corporation Ionic liquid multi-mode propulsion system
FR2976626B1 (en) * 2011-06-17 2013-07-05 Snecma CRYOGENIC PROPULSIVE ASSEMBLY
CN102926889B (en) * 2012-10-31 2015-05-27 北京控制工程研究所 Method for using bipropellants efficiently
CN103213692B (en) * 2013-04-09 2015-05-27 北京控制工程研究所 Method of actively adjusting balanced discharging of parallel connection tanks of satellite two component propelling system
FR3013773B1 (en) * 2013-11-22 2019-04-05 Arianegroup Sas DEVICE FOR SUPPLYING ERGOL FROM PROPULSIVE CHAMBER OF ENGINE-ROCKET
CN106894919A (en) * 2015-12-21 2017-06-27 北京宇航系统工程研究所 A kind of tank in parallel equilibrium induction system based on communicating pipe
US11286886B2 (en) * 2019-04-14 2022-03-29 Hamilton Sundstrand Corporation Distributed fuel modules with hydraulic flow circuit breakers and gaseous flow circuit breakers
CN112693632B (en) * 2020-12-25 2021-09-21 上海空间推进研究所 Method and system for adjusting and compensating on-orbit performance of spacecraft propulsion system

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3231223A (en) * 1962-11-16 1966-01-25 Thiokol Chemical Corp Flight attitude control system
US3807657A (en) * 1972-01-31 1974-04-30 Rca Corp Dual thrust level monopropellant spacecraft propulsion system
DE2241424C3 (en) * 1972-08-23 1978-06-22 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Method for operating a liquid rocket engine
US3923188A (en) * 1973-12-12 1975-12-02 Rca Corp Satellite propellant management system
US4741502A (en) * 1985-10-01 1988-05-03 Hughes Aircraft Company Method and apparatus for launching a spacecraft by use of a recoverable upper rocket stage
WO1987004992A1 (en) * 1986-02-18 1987-08-27 Hughes Aircraft Company Low pressure reaction control propulsion system for a spacecraft
GB8610849D0 (en) * 1986-05-02 1986-08-20 Marconi Co Ltd Gas thruster
GB2190141B (en) * 1986-05-02 1990-02-28 Marconi Co Ltd Gas thruster system for a space craft
JPH01500531A (en) * 1986-06-19 1989-02-23 ヒユーズ・エアクラフト・カンパニー Complex spacecraft control system

Also Published As

Publication number Publication date
GB2226999A (en) 1990-07-18
FR2640579B1 (en) 1994-10-07
JPH02212299A (en) 1990-08-23
DE3939910C2 (en) 1998-07-16
FR2640579A1 (en) 1990-06-22
DE3939910A1 (en) 1990-09-06
GB2226999B (en) 1992-05-27
US5263666A (en) 1993-11-23
IT8922688A0 (en) 1989-12-14
GB8927708D0 (en) 1990-02-07
CA1331596C (en) 1994-08-23

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Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19971223