FR2729117B1 - Procede de pilotage d'un engin et engin permettant la mise en oeuvre du procede - Google Patents

Procede de pilotage d'un engin et engin permettant la mise en oeuvre du procede

Info

Publication number
FR2729117B1
FR2729117B1 FR9500180A FR9500180A FR2729117B1 FR 2729117 B1 FR2729117 B1 FR 2729117B1 FR 9500180 A FR9500180 A FR 9500180A FR 9500180 A FR9500180 A FR 9500180A FR 2729117 B1 FR2729117 B1 FR 2729117B1
Authority
FR
France
Prior art keywords
machine
steering
implementing
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 - Fee Related
Application number
FR9500180A
Other languages
English (en)
Other versions
FR2729117A1 (fr
Inventor
Alain Wagner
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR9500180A priority Critical patent/FR2729117B1/fr
Priority to US08/583,481 priority patent/US6142424A/en
Priority to JP8000814A priority patent/JPH08230799A/ja
Publication of FR2729117A1 publication Critical patent/FR2729117A1/fr
Application granted granted Critical
Publication of FR2729117B1 publication Critical patent/FR2729117B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
FR9500180A 1995-01-10 1995-01-10 Procede de pilotage d'un engin et engin permettant la mise en oeuvre du procede Expired - Fee Related FR2729117B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR9500180A FR2729117B1 (fr) 1995-01-10 1995-01-10 Procede de pilotage d'un engin et engin permettant la mise en oeuvre du procede
US08/583,481 US6142424A (en) 1995-01-10 1996-01-05 Method of steering a vehicle and vehicle allowing implementation of the method
JP8000814A JPH08230799A (ja) 1995-01-10 1996-01-08 ビークル及びその操縦方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9500180A FR2729117B1 (fr) 1995-01-10 1995-01-10 Procede de pilotage d'un engin et engin permettant la mise en oeuvre du procede

Publications (2)

Publication Number Publication Date
FR2729117A1 FR2729117A1 (fr) 1996-07-12
FR2729117B1 true FR2729117B1 (fr) 1997-04-04

Family

ID=9474966

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9500180A Expired - Fee Related FR2729117B1 (fr) 1995-01-10 1995-01-10 Procede de pilotage d'un engin et engin permettant la mise en oeuvre du procede

Country Status (3)

Country Link
US (1) US6142424A (fr)
JP (1) JPH08230799A (fr)
FR (1) FR2729117B1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6622971B1 (en) * 2001-05-22 2003-09-23 Lockheed Martin Corporation Adapter for connecting rocket stages
US6695261B2 (en) * 2002-02-11 2004-02-24 The Boeing Company Shock isolation system for spacecraft fairing
FR2839550B1 (fr) * 2002-05-07 2004-07-30 Eads Launch Vehicles Dispositif de liaison provisoire et de separation pyrotechnique de deux elements, a organe mobile
US7082878B2 (en) * 2003-07-01 2006-08-01 Raytheon Company Missile with multiple nosecones
WO2005075025A1 (fr) * 2004-02-10 2005-08-18 Federal State Unitary Enterprise 'state Research And Production Enterprise 'bazalt' Procede et dispositif de localisation et/ou d'extinction d'incendie
FR2872127B1 (fr) * 2004-06-29 2006-08-11 Airbus France Sas Dispositif et procede de fixation d'un radome d'aeronef
JP5417040B2 (ja) * 2009-05-25 2014-02-12 株式会社Ihiエアロスペース スライド式フェアリング脱頭装置及びスライド式フェアリング脱頭方法
US8336826B2 (en) * 2010-07-30 2012-12-25 The Aerospace Corporation Propulsion systems and methods utilizing smart propellant
CN101995192B (zh) * 2010-08-24 2013-07-17 湖北航天技术研究院总体设计所 一种具有导向功能的头体分离装置
CN104457447B (zh) * 2014-11-06 2017-05-10 北京航天长征飞行器研究所 一种加速飞行器头体分离的装置
SE540399C2 (sv) * 2016-04-20 2018-09-11 Bae Systems Bofors Ab Stödanordning för delningsbar fallskärmsgranat
FR3076817B1 (fr) * 2018-01-16 2020-02-14 Arianegroup Sas Procede d'ejection d'une charge utile depuis un vehicule spatial anime d'une force de propulsion continue
CN109573115B (zh) * 2018-12-29 2020-09-15 湖北航天技术研究院总体设计所 整流罩开启装置
US11987398B2 (en) * 2021-09-06 2024-05-21 Pritok Capital LLC Method and apparatus for underwater launch platform for spacecraft
TR2021014519A2 (tr) * 2021-09-16 2021-09-21 Atatuerk Ueniversitesi Rektoerluegue Bilimsel Arastirma Projeleri Bap Koordinasyon Birimi Roket, füze ve uydu bi̇leşenleri̇ yayli tahli̇ye si̇stemi̇
CN113899260B (zh) * 2021-10-25 2023-01-20 航天科工火箭技术有限公司 一种整流罩的轴向分离装置以及运载火箭
GB202210042D0 (en) * 2022-07-08 2022-08-24 Raptor Aerospace Ltd Systems,assemblies and methods for payload testing

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3260204A (en) * 1964-06-08 1966-07-12 Jr John W Wilkey Velocity package
FR1499209A (fr) * 1966-07-06 1967-10-27 Snecma Dispositif de fixation et d'éjection des coiffes de fusée
US3384016A (en) * 1966-09-06 1968-05-21 Nasa Usa Lateral displacement system for separated rocket stages
GB1220994A (en) * 1968-03-07 1971-01-27 Trw Inc Band retainer for satellite separation system
US3534686A (en) * 1968-10-04 1970-10-20 Nasa Payload/burned-out motor case separation system
US3652042A (en) * 1970-12-28 1972-03-28 Trw Inc Spacecraft for deploying multiple objects
US3907225A (en) * 1973-12-17 1975-09-23 Tru Inc Spacecraft for deploying objects into selected flight paths
FR2649667B1 (fr) * 1989-07-17 1991-09-20 Centre Nat Etd Spatiales Procede de lancement dans l'espace d'une capsule et moyen de lancement correspondant
US5305974A (en) * 1991-07-23 1994-04-26 Willis Robert C Spaceship propulsion by momentum transfer

Also Published As

Publication number Publication date
US6142424A (en) 2000-11-07
FR2729117A1 (fr) 1996-07-12
JPH08230799A (ja) 1996-09-10

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ST Notification of lapse

Effective date: 20100930