DE69801309D1 - Vorrichtung zum aufhängen einer nutzlast in einer trägerrakete - Google Patents

Vorrichtung zum aufhängen einer nutzlast in einer trägerrakete

Info

Publication number
DE69801309D1
DE69801309D1 DE69801309A DE69801309A DE69801309D1 DE 69801309 D1 DE69801309 D1 DE 69801309D1 DE 69801309 A DE69801309 A DE 69801309A DE 69801309 A DE69801309 A DE 69801309A DE 69801309 D1 DE69801309 D1 DE 69801309D1
Authority
DE
Germany
Prior art keywords
suspensing
launcher
payload
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.)
Expired - Lifetime
Application number
DE69801309A
Other languages
English (en)
Other versions
DE69801309T2 (de
DE69801309T4 (de
Inventor
Marie-Dominique Hubert
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Application granted granted Critical
Publication of DE69801309D1 publication Critical patent/DE69801309D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/42—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing
    • F16F1/52—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses
    • F16F1/54—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses loaded in compression and shear
    • 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
    • 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
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/02—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum
    • F16F9/04—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum in a chamber with a flexible wall
    • F16F9/0418—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum in a chamber with a flexible wall having a particular shape, e.g. annular, spherical, tube-like
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/10—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using liquid only; using a fluid of which the nature is immaterial

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Child & Adolescent Psychology (AREA)
  • Vehicle Body Suspensions (AREA)
  • Vibration Prevention Devices (AREA)
  • Toys (AREA)
DE69801309A 1997-01-29 1998-01-29 Vorrichtung zum aufhängen einer nutzlast in einer trägerrakete Expired - Lifetime DE69801309D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9700949A FR2758791B1 (fr) 1997-01-29 1997-01-29 Dispositif de suspension d'une charge utile dans un lanceur spatial
PCT/FR1998/000167 WO1998032658A1 (fr) 1997-01-29 1998-01-29 Dispositif de suspension d'une charge utile dans un lanceur spatial

Publications (1)

Publication Number Publication Date
DE69801309D1 true DE69801309D1 (de) 2001-09-13

Family

ID=9503082

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69801309T Expired - Lifetime DE69801309T4 (de) 1997-01-29 1998-01-29 Vorrichtung zum aufhängen einer nutzlast in einer trägerrakete
DE69801309A Expired - Lifetime DE69801309D1 (de) 1997-01-29 1998-01-29 Vorrichtung zum aufhängen einer nutzlast in einer trägerrakete

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE69801309T Expired - Lifetime DE69801309T4 (de) 1997-01-29 1998-01-29 Vorrichtung zum aufhängen einer nutzlast in einer trägerrakete

Country Status (8)

Country Link
US (1) US6244541B1 (de)
EP (1) EP0956236B1 (de)
JP (1) JP2001509751A (de)
DE (2) DE69801309T4 (de)
ES (1) ES2160402T3 (de)
FR (1) FR2758791B1 (de)
RU (1) RU2203839C2 (de)
WO (1) WO1998032658A1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2787765B1 (fr) 1998-12-29 2001-02-16 Centre Nat Etd Spatiales Dispositif de support d'une charge utile dans un lanceur de ladite charge utile
FR2787764B1 (fr) 1998-12-29 2001-02-16 Centre Nat Etd Spatiales Dispositif de suspension d'une charge utile dans un lanceur spatial
US6202961B1 (en) * 2000-03-21 2001-03-20 Csa Engineering Passive, multi-axis, highly damped, shock isolation mounts for spacecraft
SE0003315L (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
US6609681B2 (en) * 2001-07-05 2003-08-26 The Boeing Company Method and apparatus for damping vibration
US6695261B2 (en) * 2002-02-11 2004-02-24 The Boeing Company Shock isolation system for spacecraft fairing
US20050109878A1 (en) * 2002-03-28 2005-05-26 Dutch Space B.V. Spacecraft and method for building such a spacecraft and an adapter to be used in such a spacecraft
US20050056509A1 (en) * 2003-09-16 2005-03-17 The Boeing Company Shock isolation system
US7222823B2 (en) * 2004-07-06 2007-05-29 Ata Engineering, Inc. Payload adapter
US7819221B1 (en) * 2005-09-27 2010-10-26 The United States Of America As Represented By The Secretary Of The Air Force Lightweight acoustic damping treatment
US7905453B2 (en) * 2006-12-21 2011-03-15 Intelsat Piggyback equipment panel payload arrangement, a device for and method of attaching a hosted secondary piggyback payload and adapter to be used for a piggyback secondary payload arrangement for launching the piggyback equipment panel secondary
US7866607B2 (en) * 2006-12-21 2011-01-11 Intelsat Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite
FR2951792B1 (fr) * 2009-10-28 2017-02-03 Airbus Operations Sas Dispositif de liaison a amortissement antivibratoire
FR2965876B1 (fr) * 2010-10-11 2013-10-18 Airbus Operations Sas Dispositif de filtrage fluide de vibrations mecaniques
JP2012131410A (ja) * 2010-12-22 2012-07-12 Mitsubishi Heavy Ind Ltd アダプタおよびペイロード打ち上げ用ロケット
JP5888671B2 (ja) * 2011-11-24 2016-03-22 株式会社Ｉｈｉエアロスペース 振動緩和装置
FR3012553B1 (fr) * 2013-10-31 2016-06-24 Astrium Sas Module d'isolation de vibrations a effets non lineaires diminues
US10214303B1 (en) * 2016-09-27 2019-02-26 Space Systems/Loral, Llc Low cost launch vehicle fairing
US10562650B2 (en) * 2017-06-28 2020-02-18 The Boeing Company Corrugated payload adaptor structure
CN109264029A (zh) * 2018-09-27 2019-01-25 宁波天擎航天科技有限公司 一种运载火箭

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB252843A (en) * 1925-04-14 1926-06-10 George Sydney Dominy Improvements relating to the supporting of road & rail vehicles and all apparatus needing isolation from vibration, by means of air under pressure
US2047963A (en) * 1933-04-25 1936-07-21 Edward L Hoffman Aircraft engine mount
US2999707A (en) * 1956-11-28 1961-09-12 Mobay Chemical Corp Flexible joint
US3222017A (en) * 1964-03-30 1965-12-07 Gen Electric Engine mounting
GB1079281A (en) * 1964-10-06 1967-08-16 Metalastik Ltd Resilient mountings and supports
JPS5447075A (en) * 1977-09-20 1979-04-13 Toshiba Corp Vibration-proof equipment
FR2426830A1 (fr) * 1978-05-22 1979-12-21 Org Europeene De Rech Dispositif a moment d'inertie a suspension magnetique
DE2838737A1 (de) * 1978-09-06 1980-03-20 Messerschmitt Boelkow Blohm Daemmelement zur schwingungsisolierung
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
US4811919A (en) * 1987-08-06 1989-03-14 Lord Corporation Volume compensated fluid mount
US4848525A (en) * 1987-11-02 1989-07-18 The Boeing Company Dual mode vibration isolator
US5244170A (en) * 1991-10-15 1993-09-14 General Dynamics Corporation, Space Systems Division Passive nonlinear interface strut (PNIS)
US5219051A (en) * 1991-10-25 1993-06-15 Honeywell Inc. Folded viscous damper
US5655757A (en) * 1995-02-17 1997-08-12 Trw Inc. Actively controlled damper
US5878980A (en) * 1997-02-05 1999-03-09 Hughes Electronics Corporation Attenuation ring
US6012680A (en) * 1997-06-27 2000-01-11 Mcdonnell Douglas Corporation Passive lateral vibration isolation system for a spacecraft launch vehicle

Also Published As

Publication number Publication date
DE69801309T2 (de) 2002-04-25
EP0956236B1 (de) 2001-08-08
FR2758791A1 (fr) 1998-07-31
EP0956236A1 (de) 1999-11-17
DE69801309T4 (de) 2003-11-20
RU2203839C2 (ru) 2003-05-10
ES2160402T3 (es) 2001-11-01
FR2758791B1 (fr) 1999-03-26
US6244541B1 (en) 2001-06-12
JP2001509751A (ja) 2001-07-24
WO1998032658A1 (fr) 1998-07-30

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Legal Events

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