DE2331607A1 - Vorrichtung zur halterung einer ladung - Google Patents
Vorrichtung zur halterung einer ladungInfo
- Publication number
- DE2331607A1 DE2331607A1 DE2331607A DE2331607A DE2331607A1 DE 2331607 A1 DE2331607 A1 DE 2331607A1 DE 2331607 A DE2331607 A DE 2331607A DE 2331607 A DE2331607 A DE 2331607A DE 2331607 A1 DE2331607 A1 DE 2331607A1
- Authority
- DE
- Germany
- Prior art keywords
- fluid
- load
- supporting structure
- devices
- space
- 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.)
- Ceased
Links
- 239000012530 fluid Substances 0.000 claims description 16
- 238000005452 bending Methods 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 4
- 241001233037 catfish Species 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Actuator (AREA)
- Transmission Devices (AREA)
- Earth Drilling (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2934572A GB1420957A (en) | 1972-06-22 | 1972-06-22 | Spacecraft |
Publications (1)
Publication Number | Publication Date |
---|---|
DE2331607A1 true DE2331607A1 (de) | 1974-01-17 |
Family
ID=10290081
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE2331607A Ceased DE2331607A1 (de) | 1972-06-22 | 1973-06-20 | Vorrichtung zur halterung einer ladung |
Country Status (4)
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5217187A (en) * | 1983-11-07 | 1993-06-08 | Criswell David R | Multi-use launch system |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4082240A (en) * | 1976-08-23 | 1978-04-04 | General Dynamics Corporation | Continuous integrated clamping hoop space vehicle support system |
US4043524A (en) * | 1976-08-23 | 1977-08-23 | General Dynamics Corporation | Support and load alleviation system for space vehicles |
US4231537A (en) * | 1978-03-22 | 1980-11-04 | Satellite Business Systems | Satellite-launch vehicle combination and method |
US4300737A (en) * | 1978-05-30 | 1981-11-17 | Hughes Aircraft Company | Satellite deployment system with remotely controlled relocking capability |
US4290570A (en) * | 1978-05-30 | 1981-09-22 | Hughes Aircraft Company | Three point attachment for an ejectable spacecraft |
US4324374A (en) * | 1978-05-30 | 1982-04-13 | Hughes Aircraft Company | Integrated spacecraft and cradle structure |
US4303214A (en) * | 1978-05-30 | 1981-12-01 | Hughes Aircraft Company | Apparatus for gyroscopic ejection of shuttle launched spacecraft |
US4359201A (en) * | 1980-02-28 | 1982-11-16 | Hughes Aircraft Company | Payload deployment from shuttle with linear and angular velocity |
US4508296A (en) * | 1982-07-23 | 1985-04-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Hemispherical latching apparatus |
GB8313864D0 (en) * | 1983-05-19 | 1983-06-22 | Garrard Products Ltd | Damping oscillatory system |
GB2140124B (en) * | 1983-05-19 | 1986-07-09 | Garrard Products | A device for damping an oscillatory system |
US4600169A (en) * | 1983-12-23 | 1986-07-15 | Hughes Aircraft Company | Integrated spacecraft cradle and shuttle structure |
US4557444A (en) * | 1984-01-09 | 1985-12-10 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aerospace vehicle |
US4618111A (en) * | 1984-05-08 | 1986-10-21 | Trw Inc. | Spacecraft structure for supporting an optical bench |
US4834325A (en) * | 1985-03-20 | 1989-05-30 | Space Industries, Inc. | Modular spacecraft system |
US4711417A (en) * | 1985-09-26 | 1987-12-08 | Hughes Aircraft Company | Apparatus for ejection of a spacecraft |
US4946116A (en) * | 1988-12-14 | 1990-08-07 | The Boeing Company | Engine mount including latch mechanism |
US5696319A (en) * | 1996-09-06 | 1997-12-09 | Mcdonnell Douglas Corporation | Flexure fixture for dynamic loading modal surveys of test articles |
RU2175932C1 (ru) * | 2001-02-07 | 2001-11-20 | Закрытое акционерное общество "Авиационная компания "Полет" | Устройство десантирования из самолета тяжелых крупногабаритных грузов |
US6644596B1 (en) * | 2001-12-21 | 2003-11-11 | Air Cruisers Company | Deployment system for inflatable structures |
DE102004016593A1 (de) * | 2004-04-03 | 2005-10-20 | Eads Space Transp Gmbh | Vorrichtung zur Übertragung von Lasten |
US7434600B1 (en) | 2004-12-02 | 2008-10-14 | Air Cruisers Company | Pressurized actuator system for inflatable structures |
US7644739B1 (en) | 2004-12-02 | 2010-01-12 | Air Cruisers Company | Pressurized actuation system for inflatable structures |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2697569A (en) * | 1952-01-17 | 1954-12-21 | Fairchild Engine & Airplane | Detachable fuselage aircraft |
US2891765A (en) * | 1955-11-25 | 1959-06-23 | Frank S Pearne | Jack |
US2998948A (en) * | 1959-07-28 | 1961-09-05 | Harold D Sisk | Cargo-carrying aircraft |
US3450376A (en) * | 1965-10-18 | 1969-06-17 | Nikolai Grigorievich Rusanovic | Device for rigid fastening of cargo to aircraft particularly to helicopter-crane for transporting this cargo |
SE318385B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * | 1969-02-13 | 1969-12-08 | B Larsson | |
US3700193A (en) * | 1971-01-14 | 1972-10-24 | Nasa | A method of delivering a vehicle to earth orbit and returning the reusable portion thereof to earth |
-
1972
- 1972-06-22 GB GB2934572A patent/GB1420957A/en not_active Expired
-
1973
- 1973-06-14 US US00369882A patent/US3815849A/en not_active Expired - Lifetime
- 1973-06-20 DE DE2331607A patent/DE2331607A1/de not_active Ceased
- 1973-06-21 FR FR7322728A patent/FR2189259B3/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5217187A (en) * | 1983-11-07 | 1993-06-08 | Criswell David R | Multi-use launch system |
Also Published As
Publication number | Publication date |
---|---|
GB1420957A (en) | 1976-01-14 |
FR2189259A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1974-01-25 |
FR2189259B3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1976-06-18 |
US3815849A (en) | 1974-06-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OD | Request for examination | ||
8131 | Rejection |