AU2002215280A1 - A construction and a method to be used in a carrier rocket or a satellit - Google Patents

A construction and a method to be used in a carrier rocket or a satellit

Info

Publication number
AU2002215280A1
AU2002215280A1 AU2002215280A AU1528002A AU2002215280A1 AU 2002215280 A1 AU2002215280 A1 AU 2002215280A1 AU 2002215280 A AU2002215280 A AU 2002215280A AU 1528002 A AU1528002 A AU 1528002A AU 2002215280 A1 AU2002215280 A1 AU 2002215280A1
Authority
AU
Australia
Prior art keywords
satellit
construction
carrier rocket
rocket
carrier
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.)
Abandoned
Application number
AU2002215280A
Inventor
Orjan Arulf
Jorgen Remmelg
Rolf Thornkvist
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RUAG Space AB
Original Assignee
SAAB Ericson 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 Ericson Space AB filed Critical SAAB Ericson Space AB
Publication of AU2002215280A1 publication Critical patent/AU2002215280A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/002Launch systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641Interstage or payload connectors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/55Member ends joined by inserted section
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/55Member ends joined by inserted section
    • Y10T403/556Section threaded to member
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/75Joints and connections having a joining piece extending through aligned openings in plural members

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
AU2002215280A 2000-11-24 2001-11-14 A construction and a method to be used in a carrier rocket or a satellit Abandoned AU2002215280A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0004310 2000-11-24
SE0004310A SE0004310L (en) 2000-11-24 2000-11-24 Design and procedure of carrier rocket or satellite
PCT/SE2001/002517 WO2002042152A1 (en) 2000-11-24 2001-11-14 A construction and a method to be used in a carrier rocket or a satellit

Publications (1)

Publication Number Publication Date
AU2002215280A1 true AU2002215280A1 (en) 2002-06-03

Family

ID=20281948

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2002215280A Abandoned AU2002215280A1 (en) 2000-11-24 2001-11-14 A construction and a method to be used in a carrier rocket or a satellit

Country Status (5)

Country Link
US (1) US6913225B2 (en)
EP (1) EP1335852A1 (en)
AU (1) AU2002215280A1 (en)
SE (1) SE0004310L (en)
WO (1) WO2002042152A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040218599A1 (en) * 2003-05-01 2004-11-04 Genesis Microchip Inc. Packet based video display interface and methods of use thereof
DE60331146D1 (en) * 2003-10-03 2010-03-18 Ruag Aerospace Sweden Ab Method for connecting a component
US7347641B2 (en) * 2004-03-31 2008-03-25 The Boeing Company Methods and systems for joining structures
US20060269357A1 (en) * 2005-05-31 2006-11-30 United Technologies Corporation Rotating shaft coupling assembly
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
US7712993B2 (en) * 2007-11-30 2010-05-11 The Boeing Company Double shear joint for bonding in structural applications
US8459596B2 (en) * 2009-12-01 2013-06-11 Sunstar IM Sky/space elevators
US9777579B2 (en) 2012-12-10 2017-10-03 General Electric Company Attachment of composite article
US9797257B2 (en) 2012-12-10 2017-10-24 General Electric Company Attachment of composite article
CN111470069B (en) * 2020-04-08 2021-11-16 上海卫星工程研究所 Lower end frame structure suitable for satellite bearing cylinder

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1167943A (en) * 1915-08-25 1916-01-11 Horace L Short Aeroplane.
US3051517A (en) * 1961-01-17 1962-08-28 Yalen Abraham Spring metal u-shaped anchor
US3556569A (en) * 1969-07-24 1971-01-19 Streater Ind Inc Connector assembly for joining tubular members at right angles
US4038118A (en) * 1974-06-14 1977-07-26 The Boeing Company Three dimensional composite structure and method for incorporating fittings
GB1469733A (en) * 1975-01-08 1977-04-06 Wong Kam Wah Method of joining a screw-threaded shank to a rattan pole
US4228631A (en) * 1978-09-12 1980-10-21 Geffe Bruce T Hollow rectangular joist
CA1209776A (en) * 1984-08-24 1986-08-19 William S. Stefnik Unitized partition system
GB8828025D0 (en) * 1988-12-01 1989-01-05 Atomic Energy Authority Uk Screw fasteners for aeronautical use
FR2648199B1 (en) * 1989-06-09 1991-09-27 Aerospatiale TEMPORARY LINK DEVICE, PARTICULARLY FOR ARTIFICIAL SATELLITE APPENDIX, AND METHOD FOR RELEASING SUCH A LINK
US5308183A (en) * 1992-07-09 1994-05-03 General Motors Corporation Lock coupling between shaft and rotor
JP2536098Y2 (en) * 1992-09-02 1997-05-21 星野楽器株式会社 Pipe fixing device
FR2718706B1 (en) * 1994-04-15 1996-06-14 Aerospatiale Anti-spark structure, especially for aircraft.
US6050033A (en) * 1997-01-31 2000-04-18 Wrightman; Ronald A. Bolted post and beam
US6012680A (en) 1997-06-27 2000-01-11 Mcdonnell Douglas Corporation Passive lateral vibration isolation system for a spacecraft launch vehicle
US5969287A (en) * 1997-12-16 1999-10-19 Lockheed Martin Corporation Separation system

Also Published As

Publication number Publication date
WO2002042152A1 (en) 2002-05-30
SE516459C2 (en) 2002-01-15
US20040061024A1 (en) 2004-04-01
EP1335852A1 (en) 2003-08-20
SE0004310L (en) 2002-01-15
US6913225B2 (en) 2005-07-05
SE0004310D0 (en) 2000-11-24

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