ATE294733T1 - Wiederverwendbare, trennbare, strukturverbindungseinrichtung und verfahren zum verbinden von zwei fahrzeugen - Google Patents

Wiederverwendbare, trennbare, strukturverbindungseinrichtung und verfahren zum verbinden von zwei fahrzeugen

Info

Publication number
ATE294733T1
ATE294733T1 AT00950196T AT00950196T ATE294733T1 AT E294733 T1 ATE294733 T1 AT E294733T1 AT 00950196 T AT00950196 T AT 00950196T AT 00950196 T AT00950196 T AT 00950196T AT E294733 T1 ATE294733 T1 AT E294733T1
Authority
AT
Austria
Prior art keywords
protrusions
band
recess
reusable
separable
Prior art date
Application number
AT00950196T
Other languages
English (en)
Inventor
Walter Holemans
Original Assignee
Walter Holemans
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 Walter Holemans filed Critical Walter Holemans
Application granted granted Critical
Publication of ATE294733T1 publication Critical patent/ATE294733T1/de

Links

Classifications

    • 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
    • B64G1/645Separators
    • 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)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Springs (AREA)
  • Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
  • Insertion Pins And Rivets (AREA)
  • Body Structure For Vehicles (AREA)
  • Storage Of Web-Like Or Filamentary Materials (AREA)
AT00950196T 1999-04-06 2000-03-02 Wiederverwendbare, trennbare, strukturverbindungseinrichtung und verfahren zum verbinden von zwei fahrzeugen ATE294733T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/287,038 US6227493B1 (en) 1999-04-06 1999-04-06 Reusable, separable, structural connector assembly
PCT/US2000/005172 WO2000059783A2 (en) 1999-04-06 2000-03-02 Reusable, separable, structural connector assembly

Publications (1)

Publication Number Publication Date
ATE294733T1 true ATE294733T1 (de) 2005-05-15

Family

ID=23101213

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00950196T ATE294733T1 (de) 1999-04-06 2000-03-02 Wiederverwendbare, trennbare, strukturverbindungseinrichtung und verfahren zum verbinden von zwei fahrzeugen

Country Status (5)

Country Link
US (3) US6227493B1 (de)
EP (1) EP1202905B1 (de)
AT (1) ATE294733T1 (de)
DE (1) DE60019933D1 (de)
WO (1) WO2000059783A2 (de)

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US20050279890A1 (en) * 2004-03-23 2005-12-22 Walter Holemans Latching separation system
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US9434485B1 (en) * 2013-01-25 2016-09-06 Stephen C. Lehocki Multi-purpose cargo delivery and space debris removal system
CN103738509A (zh) * 2014-01-21 2014-04-23 北京航空航天大学 一种新型多星分离解锁释放装置
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IL236287A0 (en) * 2014-12-15 2015-08-31 Haim Korach A system for inserting an excess launcher sheath
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FR3055887B1 (fr) * 2016-09-14 2019-06-21 Airbus Safran Launchers Sas Dispositif de liaison a separation commandee par effet thermique non pyrotechnique a temps de reaction reduit
CN107380487B (zh) * 2017-06-06 2020-11-24 上海卫星工程研究所 一体化方转圆型星箭连接环
US10669048B1 (en) * 2017-06-15 2020-06-02 United Launch Alliance, L.L.C. Mechanism for increasing jettison clearance
CN107521718B (zh) * 2017-07-04 2020-12-29 西安飞机工业(集团)有限责任公司 一种测量飞机蒙皮间密封胶收缩量的方法
EP4147981A1 (de) 2017-07-21 2023-03-15 Northrop Grumman Systems Corporation Wartungsvorrichtungen für raumfahrzeuge und zugehörige anordnungen, systeme und verfahren
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CN108715236B (zh) * 2018-03-28 2021-11-16 上海宇航系统工程研究所 模拟实现空间小型卫星可重复使用的地面试验台
CN108731958B (zh) * 2018-04-04 2019-12-27 北京强度环境研究所 一种火箭根部弯矩监测系统的电缆脱开装置
CN108423199B (zh) * 2018-04-23 2021-03-12 陕西中天火箭技术股份有限公司 一种火药作动筒式级间舱
CN109760858B (zh) * 2018-12-18 2022-08-05 上海航天控制技术研究所 二自由度解耦的空间黏附爪传动装置
EP3911574A4 (de) 2019-01-15 2022-09-14 Northrop Grumman Systems Corporation Wartungsvorrichtungen für raumfahrzeuge und zugehörige anordnungen, systeme und verfahren
RU2717930C1 (ru) * 2019-05-29 2020-03-26 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Устройство соединения корпусов отсеков
US11827386B2 (en) 2020-05-04 2023-11-28 Northrop Grumman Systems Corporation Vehicle capture assemblies and related devices, systems, and methods
US11859648B1 (en) 2020-05-08 2024-01-02 Lockheed Martin Corporation System and method for providing a joint between parts of an object without compromising structural factors of the object
FR3109928B1 (fr) * 2020-05-11 2022-04-22 Centre Nat Etd Spatiales Dispositif de déploiement amélioré pour nano-satellite
US11802606B2 (en) * 2020-05-18 2023-10-31 The Boeing Company Planate dynamic isolator
AU2021273575A1 (en) 2020-12-17 2022-07-07 The Boeing Company Satellite thermal enclosure
US11987398B2 (en) * 2021-09-06 2024-05-21 Pritok Capital LLC Method and apparatus for underwater launch platform for spacecraft
CN113772135B (zh) * 2021-09-06 2024-03-29 太原科技大学 一种气动剪切解锁机构及其应用
CN113928570B (zh) * 2021-11-19 2023-12-01 中国科学院长春光学精密机械与物理研究所 航天装置的锁紧机构
PL439888A1 (pl) 2021-12-17 2023-06-19 Sieć Badawcza Łukasiewicz - Instytut Lotnictwa Mechanizm separacji modułów, w szczególności do rakiet

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Also Published As

Publication number Publication date
EP1202905B1 (de) 2005-05-04
EP1202905A2 (de) 2002-05-08
US6390416B2 (en) 2002-05-21
US20010017337A1 (en) 2001-08-30
WO2000059783A2 (en) 2000-10-12
US6343770B2 (en) 2002-02-05
US6227493B1 (en) 2001-05-08
US20020014558A1 (en) 2002-02-07
WO2000059783A3 (en) 2001-05-03
WO2000059783B1 (en) 2001-07-05
DE60019933D1 (de) 2005-06-09

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