SE0101398D0 - Flange on a spacecraft with two separable parts - Google Patents
Flange on a spacecraft with two separable partsInfo
- Publication number
- SE0101398D0 SE0101398D0 SE0101398A SE0101398A SE0101398D0 SE 0101398 D0 SE0101398 D0 SE 0101398D0 SE 0101398 A SE0101398 A SE 0101398A SE 0101398 A SE0101398 A SE 0101398A SE 0101398 D0 SE0101398 D0 SE 0101398D0
- Authority
- SE
- Sweden
- Prior art keywords
- flange
- spacecraft
- separable parts
- reducing
- vehicle
- Prior art date
Links
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
- B64G1/64—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
- B64G1/22—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
- B64G1/645—Separators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/04—Flanged joints the flanges being connected by members tensioned in the radial plane
-
- 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)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Vibration Dampers (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Abstract
The device for reducing shock waves during launching a space vehicle (2) comprises an annular unit (5) designed to deliver a radially inward force (F) to hold together the first (3) and second (4) parts of the vehicle by means of flanges (1,6). The first flange has an annular weakening (9) for reducing the energy absorption capacity during bending inwards by the radial force.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0101398A SE517025C2 (en) | 2001-04-19 | 2001-04-19 | Flange on a spacecraft with two separable parts |
FR0204749A FR2823712B1 (en) | 2001-04-19 | 2002-04-16 | DEVICE FOR SPACE ENGINE |
US10/125,561 US6648543B2 (en) | 2001-04-19 | 2002-04-19 | Device for a space vessel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0101398A SE517025C2 (en) | 2001-04-19 | 2001-04-19 | Flange on a spacecraft with two separable parts |
Publications (3)
Publication Number | Publication Date |
---|---|
SE0101398D0 true SE0101398D0 (en) | 2001-04-19 |
SE0101398L SE0101398L (en) | 2002-04-02 |
SE517025C2 SE517025C2 (en) | 2002-04-02 |
Family
ID=20283828
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0101398A SE517025C2 (en) | 2001-04-19 | 2001-04-19 | Flange on a spacecraft with two separable parts |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2823712B1 (en) |
SE (1) | SE517025C2 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4715565A (en) * | 1986-05-27 | 1987-12-29 | Hughes Aircraft Company | Clamping connection assembly for spacecraft |
US5352061A (en) * | 1993-01-05 | 1994-10-04 | Honeywell Inc. | Anti-rotation ring joint |
US6227493B1 (en) * | 1999-04-06 | 2001-05-08 | Planetary Systems Corporation | Reusable, separable, structural connector assembly |
-
2001
- 2001-04-19 SE SE0101398A patent/SE517025C2/en not_active IP Right Cessation
-
2002
- 2002-04-16 FR FR0204749A patent/FR2823712B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2823712B1 (en) | 2006-04-28 |
FR2823712A1 (en) | 2002-10-25 |
SE0101398L (en) | 2002-04-02 |
SE517025C2 (en) | 2002-04-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |