SE0101398L - Flange on a spacecraft with two separable parts - Google Patents

Flange on a spacecraft with two separable parts

Info

Publication number
SE0101398L
SE0101398L SE0101398A SE0101398A SE0101398L SE 0101398 L SE0101398 L SE 0101398L SE 0101398 A SE0101398 A SE 0101398A SE 0101398 A SE0101398 A SE 0101398A SE 0101398 L SE0101398 L SE 0101398L
Authority
SE
Sweden
Prior art keywords
flange
spacecraft
separable parts
reducing
vehicle
Prior art date
Application number
SE0101398A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE517025C2 (en
SE0101398D0 (en
Inventor
Oerjan Arulf
Original Assignee
Saab Ericsson Space Ab
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Saab Ericsson Space Ab filed Critical Saab Ericsson Space Ab
Priority to SE0101398A priority Critical patent/SE0101398L/en
Publication of SE0101398D0 publication Critical patent/SE0101398D0/en
Publication of SE517025C2 publication Critical patent/SE517025C2/en
Publication of SE0101398L publication Critical patent/SE0101398L/en
Priority to FR0204749A priority patent/FR2823712B1/en
Priority to US10/125,561 priority patent/US6648543B2/en

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
    • B64G1/645—Separators
    • 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
    • B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
    • 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
    • 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
    • B64G1/642—Clamps, e.g. Marman clamps

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (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.
SE0101398A 2001-04-19 2001-04-19 Flange on a spacecraft with two separable parts SE0101398L (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
SE0101398A SE0101398L (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 SE0101398L (en) 2001-04-19 2001-04-19 Flange on a spacecraft with two separable parts

Publications (3)

Publication Number Publication Date
SE0101398D0 SE0101398D0 (en) 2001-04-19
SE517025C2 SE517025C2 (en) 2002-04-02
SE0101398L true SE0101398L (en) 2002-04-02

Family

ID=20283828

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0101398A SE0101398L (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) SE0101398L (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
SE517025C2 (en) 2002-04-02
SE0101398D0 (en) 2001-04-19
FR2823712A1 (en) 2002-10-25
FR2823712B1 (en) 2006-04-28

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Legal Events

Date Code Title Description
NUG Patent has lapsed