CN101670888A - 包括两对罐的捆以及包括该捆的航空发射器 - Google Patents
包括两对罐的捆以及包括该捆的航空发射器 Download PDFInfo
- Publication number
- CN101670888A CN101670888A CN200910170648A CN200910170648A CN101670888A CN 101670888 A CN101670888 A CN 101670888A CN 200910170648 A CN200910170648 A CN 200910170648A CN 200910170648 A CN200910170648 A CN 200910170648A CN 101670888 A CN101670888 A CN 101670888A
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- CN
- China
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- bundle
- jar
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- aviation
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- 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.)
- Granted
Links
- 239000003380 propellant Substances 0.000 claims abstract description 11
- 230000005484 gravity Effects 0.000 claims abstract description 4
- 230000002708 enhancing effect Effects 0.000 claims description 5
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 230000014509 gene expression Effects 0.000 description 5
- 230000003321 amplification Effects 0.000 description 3
- 238000003199 nucleic acid amplification method Methods 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- HDZGCSFEDULWCS-UHFFFAOYSA-N monomethylhydrazine Chemical compound CNN HDZGCSFEDULWCS-UHFFFAOYSA-N 0.000 description 2
- 239000004449 solid propellant Substances 0.000 description 2
- MGWGWNFMUOTEHG-UHFFFAOYSA-N 4-(3,5-dimethylphenyl)-1,3-thiazol-2-amine Chemical compound CC1=CC(C)=CC(C=2N=C(N)SC=2)=C1 MGWGWNFMUOTEHG-UHFFFAOYSA-N 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
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
- B64G1/40—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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Toys (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
- Nozzles (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
Description
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0856002A FR2935686B1 (fr) | 2008-09-08 | 2008-09-08 | Fagot comportant deux paires de reservoirs et lanceur aeroporte comportant un tel fagot |
FR0856002 | 2008-09-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101670888A true CN101670888A (zh) | 2010-03-17 |
CN101670888B CN101670888B (zh) | 2015-04-29 |
Family
ID=40651694
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200910170648.2A Expired - Fee Related CN101670888B (zh) | 2008-09-08 | 2009-09-01 | 包括两对罐的捆以及包括该捆的航空发射器 |
Country Status (7)
Country | Link |
---|---|
US (1) | US8226045B2 (zh) |
EP (1) | EP2161198B1 (zh) |
JP (1) | JP5566643B2 (zh) |
CN (1) | CN101670888B (zh) |
FR (1) | FR2935686B1 (zh) |
RU (1) | RU2509039C2 (zh) |
UA (1) | UA102064C2 (zh) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103930348A (zh) * | 2011-09-20 | 2014-07-16 | 国家空间研究中心 | 推进装置舱 |
CN110155371A (zh) * | 2019-06-03 | 2019-08-23 | 北京航空航天大学 | 一种充气喷射起飞滑翔回收的火星飞行器及其使用方法 |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140077506A1 (en) * | 2012-09-14 | 2014-03-20 | Kohler Co. | Modular configuration for an lp towable genset |
FR3008070B1 (fr) * | 2013-07-08 | 2020-11-06 | Astrium Sas | Bloc propulseur pour vehicule de lancement reutilisable |
DE102018129898B4 (de) * | 2018-11-27 | 2021-02-04 | Airbus Defence and Space GmbH | Vorrichtung zum Mitführen von Treibstoff in einem Luft- und Raumfahrzeug |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3180084A (en) * | 1961-02-13 | 1965-04-27 | Ciary Corp | Thrust device |
CN87106637A (zh) * | 1986-10-01 | 1988-04-20 | 休斯航空公司 | 发射太空船的方法和装置 |
US5533331A (en) * | 1994-05-25 | 1996-07-09 | Kaiser Marquardt, Inc. | Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same |
US5816539A (en) * | 1994-02-18 | 1998-10-06 | Lockheed Martin Corporation | Orbital assist module and interstage |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3243150A (en) * | 1964-04-09 | 1966-03-29 | Boeing Co | Aerospace vehicle and tank structure |
US3286629A (en) * | 1964-10-07 | 1966-11-22 | Jay H Laue | Multi-mission module |
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 |
RU2059858C1 (ru) * | 1993-09-14 | 1996-05-10 | Конструкторское бюро "Арсенал" им.М.В.Фрунзе | Отсек жидкостной ракетной двигательной установки космического аппарата |
RU2094333C1 (ru) * | 1995-01-12 | 1997-10-27 | Научно-производственное объединение им.С.А.Лавочкина | Ракетный летательный аппарат (его варианты) и ракетный двигатель |
US6412274B1 (en) * | 2000-06-02 | 2002-07-02 | Bwx Technologies, Inc. | Solar thermal rocket |
JP2003291899A (ja) * | 2002-04-01 | 2003-10-15 | Mitsubishi Electric Corp | 人工衛星構体 |
RU2309092C2 (ru) * | 2006-01-12 | 2007-10-27 | Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) | Орбитальный модуль-заправщик |
-
2008
- 2008-09-08 FR FR0856002A patent/FR2935686B1/fr not_active Expired - Fee Related
-
2009
- 2009-08-24 US US12/546,252 patent/US8226045B2/en not_active Expired - Fee Related
- 2009-08-26 EP EP09168706.1A patent/EP2161198B1/fr not_active Not-in-force
- 2009-09-01 CN CN200910170648.2A patent/CN101670888B/zh not_active Expired - Fee Related
- 2009-09-02 JP JP2009202304A patent/JP5566643B2/ja not_active Expired - Fee Related
- 2009-09-07 UA UAA200909208A patent/UA102064C2/uk unknown
- 2009-09-07 RU RU2009133242/11A patent/RU2509039C2/ru not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3180084A (en) * | 1961-02-13 | 1965-04-27 | Ciary Corp | Thrust device |
CN87106637A (zh) * | 1986-10-01 | 1988-04-20 | 休斯航空公司 | 发射太空船的方法和装置 |
US5816539A (en) * | 1994-02-18 | 1998-10-06 | Lockheed Martin Corporation | Orbital assist module and interstage |
US5533331A (en) * | 1994-05-25 | 1996-07-09 | Kaiser Marquardt, Inc. | Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103930348A (zh) * | 2011-09-20 | 2014-07-16 | 国家空间研究中心 | 推进装置舱 |
CN103930348B (zh) * | 2011-09-20 | 2016-08-24 | 国家空间研究中心 | 推进装置舱 |
CN110155371A (zh) * | 2019-06-03 | 2019-08-23 | 北京航空航天大学 | 一种充气喷射起飞滑翔回收的火星飞行器及其使用方法 |
Also Published As
Publication number | Publication date |
---|---|
US20100059630A1 (en) | 2010-03-11 |
UA102064C2 (uk) | 2013-06-10 |
US8226045B2 (en) | 2012-07-24 |
CN101670888B (zh) | 2015-04-29 |
JP5566643B2 (ja) | 2014-08-06 |
FR2935686B1 (fr) | 2010-09-24 |
RU2509039C2 (ru) | 2014-03-10 |
EP2161198A1 (fr) | 2010-03-10 |
RU2009133242A (ru) | 2011-03-20 |
JP2010064735A (ja) | 2010-03-25 |
FR2935686A1 (fr) | 2010-03-12 |
EP2161198B1 (fr) | 2014-02-19 |
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Legal Events
Date | Code | Title | Description |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CP03 | Change of name, title or address |
Address after: Paris France Patentee after: ARIANEGROUP S.A.S. Address before: French Yixilaimu Leo Patentee before: Airbus Safran Launcher JSC |
|
CP03 | Change of name, title or address | ||
TR01 | Transfer of patent right |
Effective date of registration: 20180514 Address after: French Yixilaimu Leo Patentee after: Airbus Safran Launcher JSC Address before: Paris France Patentee before: Snecma |
|
TR01 | Transfer of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150429 Termination date: 20190901 |
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CF01 | Termination of patent right due to non-payment of annual fee |