DE3674207D1 - Niederdruckreaktions-antriebssystem fuer raumfahrzeug. - Google Patents

Niederdruckreaktions-antriebssystem fuer raumfahrzeug.

Info

Publication number
DE3674207D1
DE3674207D1 DE8787900382T DE3674207T DE3674207D1 DE 3674207 D1 DE3674207 D1 DE 3674207D1 DE 8787900382 T DE8787900382 T DE 8787900382T DE 3674207 T DE3674207 T DE 3674207T DE 3674207 D1 DE3674207 D1 DE 3674207D1
Authority
DE
Germany
Prior art keywords
low pressure
drive system
pressure reaction
space vehicle
reaction 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
DE8787900382T
Other languages
English (en)
Inventor
L Apfel
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.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Application granted granted Critical
Publication of DE3674207D1 publication Critical patent/DE3674207D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26Guiding or controlling apparatus, e.g. for attitude control using jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/401Liquid propellant rocket engines
DE8787900382T 1986-02-18 1986-11-17 Niederdruckreaktions-antriebssystem fuer raumfahrzeug. Expired - Fee Related DE3674207D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US83030686A 1986-02-18 1986-02-18
PCT/US1986/002458 WO1987004992A1 (en) 1986-02-18 1986-11-17 Low pressure reaction control propulsion system for a spacecraft

Publications (1)

Publication Number Publication Date
DE3674207D1 true DE3674207D1 (de) 1990-10-18

Family

ID=25256716

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787900382T Expired - Fee Related DE3674207D1 (de) 1986-02-18 1986-11-17 Niederdruckreaktions-antriebssystem fuer raumfahrzeug.

Country Status (6)

Country Link
EP (1) EP0257040B1 (de)
JP (1) JPH0723120B2 (de)
CN (1) CN1021470C (de)
CA (1) CA1323352C (de)
DE (1) DE3674207D1 (de)
WO (1) WO1987004992A1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636095A1 (fr) * 1988-09-05 1990-03-09 Aerospatiale Systeme d'alimentation en au moins un ergol liquide des propulseurs d'un satellite artificiel
US5263666A (en) * 1988-12-16 1993-11-23 General Electric Co. Spacecraft with increased stationkeeping fuel load
US5282357A (en) * 1990-04-19 1994-02-01 Trw Inc. High-performance dual-mode integral propulsion system
FR2697587B1 (fr) * 1992-11-04 1995-01-20 Europ Propulsion Système optimisé d'alimentation de moteur fusée réallumable.
FR2822193B1 (fr) * 2001-03-16 2003-06-27 Snecma Moteurs Module de propulsion cryotechnique a faible poussee
CN101737199A (zh) * 2008-11-10 2010-06-16 北京航空航天大学 落压式火箭发动机液体推进剂输送系统
CN102029981B (zh) * 2009-09-29 2014-12-10 李开超 四种机动车用火箭及制动系统
CN102120443A (zh) * 2010-01-12 2011-07-13 徐清华 爆炸反冲模块用于喷气动力机车制动、飞机应急着落及用于矩阵多弹头发射的方法及结构
RU2477245C2 (ru) * 2011-04-08 2013-03-10 Открытое акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Способ регулирования и стабилизации давления в рабочих установках сильфонного типа
CN102358437B (zh) * 2011-08-08 2013-11-20 北京控制工程研究所 高轨道卫星平台10n推力器布局方法
FR2994587B1 (fr) * 2012-08-20 2017-07-07 Snecma Allumeur bimodal et procede d'injection bimodale pour allumeur de moteur-fusee
CN102926889B (zh) * 2012-10-31 2015-05-27 北京控制工程研究所 一种高效利用双组元推进剂的方法
CN105299461B (zh) * 2014-07-22 2017-11-24 北京强度环境研究所 液体运载火箭模拟燃料增压加泄配气控制台
CN104309562A (zh) * 2014-10-25 2015-01-28 陈恒兰 车用准固液推进剂火箭防护系统
CN106894919A (zh) * 2015-12-21 2017-06-27 北京宇航系统工程研究所 一种基于连通管的并联贮箱均衡输送系统
CN106121866B (zh) * 2016-08-18 2017-12-29 湖北三江航天红林探控有限公司 基于压力自稳定设计的分时点火控制算法及系统
WO2019018826A1 (en) 2017-07-21 2019-01-24 Nicholson James Garret SPACE VEHICLE MAINTENANCE DEVICES AND ASSEMBLIES, SYSTEMS, AND ASSOCIATED METHODS
US11492148B2 (en) 2019-01-15 2022-11-08 Northrop Grumman Systems Corporation Spacecraft servicing pods configured to perform servicing operations on target spacecraft and related devices, assemblies, systems, and methods
MA47560B1 (fr) * 2019-12-03 2021-08-31 Taoufik Hicham Propulseur à impulsions séquentielles
US11827386B2 (en) 2020-05-04 2023-11-28 Northrop Grumman Systems Corporation Vehicle capture assemblies and related devices, systems, and methods
CN111636980B (zh) * 2020-05-15 2021-06-18 大连理工大学 一种液体推进剂波纹管式贮箱
US20220204188A1 (en) * 2020-10-16 2022-06-30 Swarm Technologies, Inc. Propulsion system for satellites
KR20230139590A (ko) * 2022-03-28 2023-10-05 (주)이노스페이스 롤제어 추력기와 이것이 구비된 하이브리드 로켓

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3300981A (en) * 1965-01-07 1967-01-31 James E Webb Zero gravity starting means for liquid propellant motors
FR2063672A5 (de) * 1969-10-27 1971-07-09 Europ Propulsion
DE7012543U (de) * 1970-04-07 1970-07-30 Kienzle Apparate Gmbh Elektrischer geber fuer streckenzaehlwerke und geschwindigkeitsmessgeraete.
US3772675A (en) * 1972-05-15 1973-11-13 Singer Co Magnetic analog-to-digital encoder
US4258546A (en) * 1979-01-15 1981-03-31 Rockwell International Corporation Propulsion system
JPS5798801A (en) * 1980-12-11 1982-06-19 Nomura Seisakusho:Kk Detecting device for rotational angle of turn table

Also Published As

Publication number Publication date
CA1323352C (en) 1993-10-19
JPS63502339A (ja) 1988-09-08
JPH0723120B2 (ja) 1995-03-15
CN87100656A (zh) 1988-08-24
EP0257040B1 (de) 1990-09-12
CN1021470C (zh) 1993-06-30
EP0257040A1 (de) 1988-03-02
WO1987004992A1 (en) 1987-08-27

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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