JPH0581479B2 - - Google Patents
Info
- Publication number
- JPH0581479B2 JPH0581479B2 JP87505470A JP50547087A JPH0581479B2 JP H0581479 B2 JPH0581479 B2 JP H0581479B2 JP 87505470 A JP87505470 A JP 87505470A JP 50547087 A JP50547087 A JP 50547087A JP H0581479 B2 JPH0581479 B2 JP H0581479B2
- Authority
- JP
- Japan
- Prior art keywords
- spacecraft
- propellant
- tank
- orbit
- fuel
- 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 - Lifetime
Links
- 239000003380 propellant Substances 0.000 description 133
- 239000000446 fuel Substances 0.000 description 76
- 239000007800 oxidant agent Substances 0.000 description 76
- 239000007789 gas Substances 0.000 description 53
- 238000000034 method Methods 0.000 description 47
- 239000007788 liquid Substances 0.000 description 45
- 238000002485 combustion reaction Methods 0.000 description 32
- 238000012546 transfer Methods 0.000 description 29
- 230000008569 process Effects 0.000 description 18
- 230000032258 transport Effects 0.000 description 17
- 238000011084 recovery Methods 0.000 description 14
- 239000002828 fuel tank Substances 0.000 description 12
- 230000015654 memory Effects 0.000 description 11
- 230000005486 microgravity Effects 0.000 description 10
- 230000001590 oxidative effect Effects 0.000 description 10
- 238000010586 diagram Methods 0.000 description 9
- 230000009977 dual effect Effects 0.000 description 7
- 238000005070 sampling Methods 0.000 description 7
- DDMOUSALMHHKOS-UHFFFAOYSA-N 1,2-dichloro-1,1,2,2-tetrafluoroethane Chemical compound FC(F)(Cl)C(F)(F)Cl DDMOUSALMHHKOS-UHFFFAOYSA-N 0.000 description 6
- 230000001133 acceleration Effects 0.000 description 5
- 230000001174 ascending effect Effects 0.000 description 5
- 238000010304 firing Methods 0.000 description 5
- 238000009987 spinning Methods 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 4
- 239000001307 helium Substances 0.000 description 4
- 229910052734 helium Inorganic materials 0.000 description 4
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 4
- 238000005259 measurement Methods 0.000 description 4
- RFCAUADVODFSLZ-UHFFFAOYSA-N 1-Chloro-1,1,2,2,2-pentafluoroethane Chemical compound FC(F)(F)C(F)(F)Cl RFCAUADVODFSLZ-UHFFFAOYSA-N 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 230000003213 activating effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 2
- 238000012937 correction Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- WFPZPJSADLPSON-UHFFFAOYSA-N dinitrogen tetraoxide Chemical compound [O-][N+](=O)[N+]([O-])=O WFPZPJSADLPSON-UHFFFAOYSA-N 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- YMHOBZXQZVXHBM-UHFFFAOYSA-N 2,5-dimethoxy-4-bromophenethylamine Chemical compound COC1=CC(CCN)=C(OC)C=C1Br YMHOBZXQZVXHBM-UHFFFAOYSA-N 0.000 description 1
- 241000545067 Venus Species 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- HDZGCSFEDULWCS-UHFFFAOYSA-N monomethylhydrazine Chemical compound CNN HDZGCSFEDULWCS-UHFFFAOYSA-N 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
-
- 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
- B64G1/2427—Transfer orbits
-
- 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
-
- 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
- B64G1/4022—Arrangements of tanks in or on spacecraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
- B64G1/006—Reusable launch rockets or boosters
-
- 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
- B64G1/2425—Geosynchronous orbits
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Plasma & Fusion (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Testing Of Engines (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/914,103 US4741502A (en) | 1985-10-01 | 1986-10-01 | Method and apparatus for launching a spacecraft by use of a recoverable upper rocket stage |
| US914,103 | 1986-10-01 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH01501133A JPH01501133A (ja) | 1989-04-20 |
| JPH0581479B2 true JPH0581479B2 (enExample) | 1993-11-12 |
Family
ID=25433925
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP62505470A Granted JPH01501133A (ja) | 1986-10-01 | 1987-08-28 | 回収可能なロケット上段を使用して宇宙航行体を打上げる方法および装置 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4741502A (enExample) |
| EP (1) | EP0287582B1 (enExample) |
| JP (1) | JPH01501133A (enExample) |
| CN (1) | CN1004998B (enExample) |
| DE (1) | DE3767879D1 (enExample) |
| WO (1) | WO1988002332A1 (enExample) |
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5263666A (en) * | 1988-12-16 | 1993-11-23 | General Electric Co. | Spacecraft with increased stationkeeping fuel load |
| US5417049A (en) * | 1990-04-19 | 1995-05-23 | Trw Inc. | Satellite propulsion and power system |
| FR2691425B1 (fr) * | 1992-05-25 | 1997-03-28 | Aerospatiale | Carenage anti-vibrations pour un groupe d'accessoires juxtaposes embarques sur un engin spatial tel qu'un lanceur. |
| US5568904A (en) * | 1992-08-28 | 1996-10-29 | Space Systems/Loral, Inc. | Steered perigee velocity augmentation |
| US5681011A (en) * | 1993-08-24 | 1997-10-28 | Orbital Sciences Corporation | Method for injecting payloads into orbit |
| US5816539A (en) * | 1994-02-18 | 1998-10-06 | Lockheed Martin Corporation | Orbital assist module and interstage |
| US5595360A (en) * | 1994-03-25 | 1997-01-21 | Hughes Aircraft Company | Optimal transfer orbit trajectory using electric propulsion |
| US5788179A (en) * | 1996-10-29 | 1998-08-04 | Mcdonnell Douglas Corporation | Missile stage ignition delay timing for axial guidance correction |
| FR2768399B1 (fr) * | 1997-09-12 | 1999-11-12 | Aerospatiale | Procede de mise sur orbite geostationnaire d'un satellite artificiel |
| US5924648A (en) * | 1997-10-03 | 1999-07-20 | Lockheed Martin Corporation | System for upending/reclining launch vehicles |
| JP4569355B2 (ja) * | 2005-03-31 | 2010-10-27 | 株式会社Ihi | スピン衛星における物体分離時の液体移動防止方法及び装置 |
| US7575200B2 (en) * | 2005-09-07 | 2009-08-18 | The Boeing Company | Space depot for spacecraft resupply |
| US7559509B1 (en) * | 2007-02-12 | 2009-07-14 | Thomas C. Taylor | Large cryogenic tank logistics for in-space vehicles |
| FR2935686B1 (fr) * | 2008-09-08 | 2010-09-24 | Snecma | Fagot comportant deux paires de reservoirs et lanceur aeroporte comportant un tel fagot |
| US8429894B2 (en) * | 2008-09-22 | 2013-04-30 | Pratt & Whitney Rocketdyne, Inc. | Nano-grained aluminum alloy bellows |
| FR2940248B1 (fr) | 2008-12-22 | 2011-02-11 | Astrium Sas | Module reutilisable pour lanceur |
| FR2961179B1 (fr) * | 2010-06-14 | 2012-07-27 | Astrium Sas | Module reutilisable simplifie pour lanceur |
| RU2438932C2 (ru) * | 2010-11-09 | 2012-01-10 | Александр Михайлович Гультяев | Ракета |
| FR2972423B1 (fr) * | 2011-03-09 | 2014-01-31 | Astrium Sas | Procede et systeme de lancement d'un satellite |
| WO2014120526A2 (en) * | 2013-01-29 | 2014-08-07 | Howells Andrew Stephen | Enhanced rocket engine fueling systems and methods |
| FR3008070B1 (fr) * | 2013-07-08 | 2020-11-06 | Astrium Sas | Bloc propulseur pour vehicule de lancement reutilisable |
| CN103662095B (zh) * | 2013-12-20 | 2015-08-19 | 北京控制工程研究所 | 一种用于双组元姿控推力器的喷注器 |
| CN104034481B (zh) * | 2014-05-07 | 2015-07-01 | 北京空间飞行器总体设计部 | 一种贮箱分布安装的航天器用推进剂配重方法 |
| CN104260901B (zh) * | 2014-09-11 | 2016-08-24 | 上海卫星工程研究所 | 模块化的双组元推进系统 |
| CN104260903B (zh) * | 2014-09-16 | 2016-05-11 | 上海卫星工程研究所 | 具备独立高轨卫星平台功能的推进舱结构 |
| CN104679012B (zh) * | 2015-02-27 | 2017-08-25 | 福建工程学院 | 基于增量权值的无人机舵量控制信息的融合方法 |
| RU2586942C1 (ru) * | 2015-03-11 | 2016-06-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") | Система отделения космического аппарата и способ ее сборки и установки |
| FR3060117B1 (fr) * | 2016-12-09 | 2019-08-16 | Airbus Defence And Space Sas | Procede de jaugeage thermique du reservoir d’un vehicule spatial et vehicule spatial equipe de moyens pour la mise en œuvre d’un tel procede |
| US11273932B2 (en) | 2017-09-10 | 2022-03-15 | Space Arena, Inc. | Enclosures for facilitating activities in space, and associated systems and methods |
| US11358739B2 (en) | 2017-09-10 | 2022-06-14 | Orbit Fab, Inc. | Systems and methods for delivering, storing, and processing materials in space |
| CN107792399A (zh) * | 2017-09-25 | 2018-03-13 | 上海卫星工程研究所 | 贮箱下探式卫星平台结构 |
| US11034235B2 (en) * | 2017-12-06 | 2021-06-15 | Orbit Fab, Inc. | Systems and methods for creating and automating an enclosed volume with a flexible fuel tank and propellant metering for machine operations |
| KR102101659B1 (ko) * | 2018-11-29 | 2020-04-17 | (주)이노스페이스 | 전기모터 구동식 산화제 펌프를 사용하는 하이브리드 로켓엔진 |
| CN114201846B (zh) * | 2020-09-18 | 2024-11-08 | 北京天兵科技有限公司 | 一种回收火箭控制中的质量估计方法 |
| US12110133B2 (en) * | 2022-04-06 | 2024-10-08 | Maxar Space Llc | Spacecraft propellant loading system |
| CN119197208B (zh) * | 2024-12-02 | 2025-02-18 | 鲁东大学 | 一种海上回收火箭封固装置及其使用方法 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1114414A (en) * | 1964-06-18 | 1968-05-22 | British Aircraft Corp Ltd | Improvements in space vehicles |
| FR2569162A1 (fr) * | 1977-11-25 | 1986-02-21 | Ford Aerospace & Communication | Procede de mise sur orbite de satellites et de vaisseaux spatiaux |
| GB2051246B (en) * | 1979-04-25 | 1983-01-26 | British Aerospace | Propellant feed system |
| US4471926A (en) * | 1979-10-29 | 1984-09-18 | Trw Inc. | Transfer vehicle for use in conjunction with a reusable space shuttle |
| US4575029A (en) * | 1979-10-30 | 1986-03-11 | Trw Inc. | Spacecraft for use in conjunction with a reusable space shuttle |
| FR2524938A1 (fr) * | 1982-04-08 | 1983-10-14 | Centre Nat Etd Spatiales | Procede de regulation du rapport de melange des propergols pour un moteur a propergols liquides par mesure des debits et regulateurs pour sa mise en oeuvre |
| US4609169A (en) * | 1984-08-14 | 1986-09-02 | The United States Of America As Represented By The Secretary Of The Air Force | Propellant tank resupply system |
| US4699339A (en) * | 1985-03-01 | 1987-10-13 | Hughes Aircraft Company | Apparatus and method for transporting a spacecraft and a fluid propellant from the earth to a substantially low gravity environment above the earth |
| JPS63500820A (ja) * | 1985-10-01 | 1988-03-24 | ヒユ−ズ・エアクラフト・カンパニ− | 宇宙船のロケットエンジンの液体２元推進剤の使用制御方法 |
-
1986
- 1986-10-01 US US06/914,103 patent/US4741502A/en not_active Expired - Lifetime
-
1987
- 1987-08-28 JP JP62505470A patent/JPH01501133A/ja active Granted
- 1987-08-28 DE DE8787905989T patent/DE3767879D1/de not_active Expired - Fee Related
- 1987-08-28 WO PCT/US1987/002112 patent/WO1988002332A1/en not_active Ceased
- 1987-08-28 EP EP87905989A patent/EP0287582B1/en not_active Expired
- 1987-09-30 CN CN87106637.8A patent/CN1004998B/zh not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPH01501133A (ja) | 1989-04-20 |
| CN87106637A (zh) | 1988-04-20 |
| US4741502A (en) | 1988-05-03 |
| WO1988002332A1 (en) | 1988-04-07 |
| DE3767879D1 (de) | 1991-03-07 |
| EP0287582A1 (en) | 1988-10-26 |
| EP0287582B1 (en) | 1991-01-30 |
| CN1004998B (zh) | 1989-08-16 |
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