FR2787764B1 - Dispositif de suspension d'une charge utile dans un lanceur spatial - Google Patents

Dispositif de suspension d'une charge utile dans un lanceur spatial

Info

Publication number
FR2787764B1
FR2787764B1 FR9816561A FR9816561A FR2787764B1 FR 2787764 B1 FR2787764 B1 FR 2787764B1 FR 9816561 A FR9816561 A FR 9816561A FR 9816561 A FR9816561 A FR 9816561A FR 2787764 B1 FR2787764 B1 FR 2787764B1
Authority
FR
France
Prior art keywords
payload
suspending
space launcher
launcher
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.)
Expired - Lifetime
Application number
FR9816561A
Other languages
English (en)
Other versions
FR2787764A1 (fr
Inventor
Pascal 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
Priority to FR9816561A priority Critical patent/FR2787764B1/fr
Priority to EP99964726A priority patent/EP1140628A1/fr
Priority to US09/868,641 priority patent/US6588707B1/en
Priority to PCT/FR1999/003302 priority patent/WO2000038987A1/fr
Priority to JP2000590911A priority patent/JP2002533268A/ja
Publication of FR2787764A1 publication Critical patent/FR2787764A1/fr
Application granted granted Critical
Publication of FR2787764B1 publication Critical patent/FR2787764B1/fr
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
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
    • 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
    • F16F2230/00—Purpose; Design features
    • F16F2230/18—Control arrangements
FR9816561A 1998-12-29 1998-12-29 Dispositif de suspension d'une charge utile dans un lanceur spatial Expired - Lifetime FR2787764B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR9816561A FR2787764B1 (fr) 1998-12-29 1998-12-29 Dispositif de suspension d'une charge utile dans un lanceur spatial
EP99964726A EP1140628A1 (fr) 1998-12-29 1999-12-28 Dispositif de suspension d'une charge utile dans un lanceur spatial
US09/868,641 US6588707B1 (en) 1998-12-29 1999-12-28 Device for suspending a payload in a launch vehicle
PCT/FR1999/003302 WO2000038987A1 (fr) 1998-12-29 1999-12-28 Dispositif de suspension d'une charge utile dans un lanceur spatial
JP2000590911A JP2002533268A (ja) 1998-12-29 1999-12-28 打上げビークルにペイロードを懸架するための装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9816561A FR2787764B1 (fr) 1998-12-29 1998-12-29 Dispositif de suspension d'une charge utile dans un lanceur spatial

Publications (2)

Publication Number Publication Date
FR2787764A1 FR2787764A1 (fr) 2000-06-30
FR2787764B1 true FR2787764B1 (fr) 2001-02-16

Family

ID=9534607

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9816561A Expired - Lifetime FR2787764B1 (fr) 1998-12-29 1998-12-29 Dispositif de suspension d'une charge utile dans un lanceur spatial

Country Status (5)

Country Link
US (1) US6588707B1 (fr)
EP (1) EP1140628A1 (fr)
JP (1) JP2002533268A (fr)
FR (1) FR2787764B1 (fr)
WO (1) WO2000038987A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE515850C2 (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
CN100436261C (zh) * 2006-08-25 2008-11-26 郑钢铁 卫星整体减振隔振装置
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
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
US9828117B2 (en) * 2016-02-04 2017-11-28 United Launch Alliance, L.L.C. Tensioning apparatus and system for clamping joints
CN106184827B (zh) * 2016-07-19 2018-05-29 哈尔滨工业大学 主被动一体式整星隔振装置
US10562650B2 (en) * 2017-06-28 2020-02-18 The Boeing Company Corrugated payload adaptor structure

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2614896A (en) * 1950-05-06 1952-10-21 Pierce Mary Brush Adjustable dampening bearing support
US4536114A (en) * 1983-07-01 1985-08-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable length strut with longitudinal compliance and locking capability
US4776539A (en) * 1985-10-10 1988-10-11 Orbital Research Partners, L.P. Cradle apparatus for supporting payloads in a space vehicle
US5226616A (en) * 1991-10-17 1993-07-13 General Dynamics Corporation, Space Systems Div. Multi-position support structure connecting a payload to a booster rocket
US5655757A (en) * 1995-02-17 1997-08-12 Trw Inc. Actively controlled damper
FR2758791B1 (fr) * 1997-01-29 1999-03-26 Centre Nat Etd Spatiales Dispositif de suspension d'une charge utile dans un lanceur spatial
US6345788B1 (en) * 1999-05-27 2002-02-12 Trw Inc. Composite structure element with built-in damping
US6357699B1 (en) * 2000-05-25 2002-03-19 The Boeing Company Device for controlled release of tension

Also Published As

Publication number Publication date
US6588707B1 (en) 2003-07-08
EP1140628A1 (fr) 2001-10-10
JP2002533268A (ja) 2002-10-08
WO2000038987A1 (fr) 2000-07-06
FR2787764A1 (fr) 2000-06-30

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