AU2085399A - Separation system - Google Patents

Separation system

Info

Publication number
AU2085399A
AU2085399A AU20853/99A AU2085399A AU2085399A AU 2085399 A AU2085399 A AU 2085399A AU 20853/99 A AU20853/99 A AU 20853/99A AU 2085399 A AU2085399 A AU 2085399A AU 2085399 A AU2085399 A AU 2085399A
Authority
AU
Australia
Prior art keywords
separation system
separation
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
AU20853/99A
Inventor
Jim W. Blain
Duane D. Grosskrueger
Michael D. Krohn
Robert Arthur Nelson
John J Smith
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.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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
Priority claimed from US08/999,572 external-priority patent/US5983802A/en
Priority claimed from US08/991,225 external-priority patent/US5992328A/en
Priority claimed from US08/999,573 external-priority patent/US5969287A/en
Application filed by Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of AU2085399A publication Critical patent/AU2085399A/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • F42B15/38—Ring-shaped explosive elements for the separation of rocket parts
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • G01C19/5607—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating tuning forks
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00—Testing or calibrating of apparatus or devices covered by the preceding groups
    • G01P21/02—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Laminated Bodies (AREA)
  • Processing Of Stones Or Stones Resemblance Materials (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
AU20853/99A 1997-12-16 1998-11-25 Separation system Abandoned AU2085399A (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US08/999,572 US5983802A (en) 1997-12-16 1997-12-16 Separation system
US08991225 1997-12-16
US08/991,225 US5992328A (en) 1997-12-16 1997-12-16 Separation system
US08/999,573 US5969287A (en) 1997-12-16 1997-12-16 Separation system
US08999573 1997-12-16
US08999572 1997-12-16
PCT/US1998/025159 WO1999031455A1 (en) 1997-12-16 1998-11-25 Separation system

Publications (1)

Publication Number Publication Date
AU2085399A true AU2085399A (en) 1999-07-05

Family

ID=27420783

Family Applications (1)

Application Number Title Priority Date Filing Date
AU20853/99A Abandoned AU2085399A (en) 1997-12-16 1998-11-25 Separation system

Country Status (5)

Country Link
EP (1) EP1040312A4 (en)
JP (1) JP2002508502A (en)
CN (1) CN1090312C (en)
AU (1) AU2085399A (en)
WO (1) WO1999031455A1 (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2805245A1 (en) * 2000-02-23 2001-08-24 Centre Nat Etd Spatiales Method of lauching a number of communication satellites mounted on the same launch platform, includes mounting satellites on bases around a launch platform and launching them simultaneously
US7367738B2 (en) * 2002-09-23 2008-05-06 The Boeing Company Apparatus and method for releaseably joining elements
JP5728820B2 (en) * 2010-04-08 2015-06-03 株式会社Ihi rocket
FR2969748B1 (en) * 2010-12-22 2013-01-25 Astrium Sas REVERSIBLE DETONATING PYROTECHNIC RUPTURE PIECE
CN102700715A (en) * 2012-06-12 2012-10-03 河南师范大学 Quick disconnection device for escape
CN103700983B (en) * 2012-09-27 2016-06-22 上海宇航系统工程研究所 Air-conditioning adapter
FR3009284B1 (en) * 2013-08-01 2017-06-09 Astrium Sas METHOD AND DEVICE FOR BINDING AND SEPARATING TWO ELEMENTS WITH MIXED BONDING AND SEPARATION MEANS
FR3040693B1 (en) * 2015-09-03 2018-08-10 Arianegroup Sas METHOD FOR LINKING AND LINEAR SEPARATING TWO ELEMENTS
CN106403734A (en) * 2016-06-17 2017-02-15 哈尔滨工程大学 Low-shock line type explosion unlocking device
CN106123709B (en) * 2016-08-16 2024-07-16 深圳光启空间技术有限公司 Aircraft interstage separation device
CN107585329A (en) * 2017-08-10 2018-01-16 大连理工大学 A kind of carrier rocket wire type bundlees separator
CN107521723A (en) * 2017-08-25 2017-12-29 北京电子工程总体研究所 A kind of linear firer's separator
CN108750149B (en) * 2018-06-15 2020-07-28 上海卫星工程研究所 Ring type connecting and separating device based on punching separation technology
CN110920899B (en) * 2019-12-05 2023-06-09 江西洪都航空工业集团有限责任公司 General cocoon type storage and transportation transmitting box for airborne equipment
CN113566659B (en) * 2020-04-29 2024-01-16 大连理工大学 Transverse-longitudinal separation integrated interstage line type separation device and application thereof
CN113834387B (en) * 2021-09-17 2023-06-06 北京宇航系统工程研究所 Large-diameter combined high-reliability expansion pipe-groove plate separation device

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3230885A (en) * 1963-01-23 1966-01-25 Thiokol Chemical Corp Explosive separation device
US3373686A (en) * 1965-03-01 1968-03-19 Lockheed Aircraft Corp Explosive actuator
US3453960A (en) * 1967-12-11 1969-07-08 Gen Dynamics Corp Noncontaminating linear explosive separation
US3486410A (en) * 1968-04-18 1969-12-30 Mc Donnell Douglas Corp Explosive severance means
US3698281A (en) * 1970-02-27 1972-10-17 Lockheed Aircraft Corp Explosive system
US4137848A (en) * 1975-11-05 1979-02-06 The United States Of America As Represented By The Secretary Of The Navy Rocket engine mount
US4685376A (en) * 1985-06-24 1987-08-11 Mcdonnell Douglas Corporation Separation system
US5109749A (en) * 1988-10-25 1992-05-05 Oea, Inc. Explosively actuated separable structure
US5046426A (en) * 1989-10-31 1991-09-10 The Boeing Company Sequential structural separation system
FR2665951B1 (en) * 1990-08-20 1992-11-13 Aerospatiale BREAKABLE CONNECTION SYSTEM FOR SEPARATING PARTS BY MEANS OF A DETONATING LOAD.
US5390606A (en) * 1992-11-02 1995-02-21 Orbital Sciences Corporation Frangible joint separation system
US5331894A (en) * 1993-06-25 1994-07-26 The Ensign-Bickford Company Explosive release coupling
US5392684A (en) * 1993-06-25 1995-02-28 The Ensign-Bickford Company Explosive thrust-producing coupling
US5372071A (en) * 1993-07-13 1994-12-13 Tracor, Inc. Thrusting separation system
US5529264A (en) * 1994-02-18 1996-06-25 Lockheed Missiles & Space Company, Inc. Launch vehicle system

Also Published As

Publication number Publication date
EP1040312A4 (en) 2002-09-04
CN1282415A (en) 2001-01-31
WO1999031455A1 (en) 1999-06-24
CN1090312C (en) 2002-09-04
JP2002508502A (en) 2002-03-19
EP1040312A1 (en) 2000-10-04

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase