DE3767879D1 - Verfahren und vorrichtung zum ausstoss eines raumfahrzeugs mit hilfe eines oberen wiederverwendbaren raketentriebwerts. - Google Patents
Verfahren und vorrichtung zum ausstoss eines raumfahrzeugs mit hilfe eines oberen wiederverwendbaren raketentriebwerts.Info
- Publication number
- DE3767879D1 DE3767879D1 DE8787905989T DE3767879T DE3767879D1 DE 3767879 D1 DE3767879 D1 DE 3767879D1 DE 8787905989 T DE8787905989 T DE 8787905989T DE 3767879 T DE3767879 T DE 3767879T DE 3767879 D1 DE3767879 D1 DE 3767879D1
- Authority
- DE
- Germany
- Prior art keywords
- output
- rocket motor
- space vehicle
- reusable rocket
- top reusable
- 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
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
- F02K9/42—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 |
| PCT/US1987/002112 WO1988002332A1 (en) | 1986-10-01 | 1987-08-28 | A method and apparatus for launching a spacecraft by use of a recoverable upper rocket stage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE3767879D1 true DE3767879D1 (de) | 1991-03-07 |
Family
ID=25433925
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE8787905989T Expired - Fee Related DE3767879D1 (de) | 1986-10-01 | 1987-08-28 | Verfahren und vorrichtung zum ausstoss eines raumfahrzeugs mit hilfe eines oberen wiederverwendbaren raketentriebwerts. |
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 |
| EP0287582A1 (en) | 1988-10-26 |
| JPH0581479B2 (enExample) | 1993-11-12 |
| EP0287582B1 (en) | 1991-01-30 |
| CN1004998B (zh) | 1989-08-16 |
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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 |