JPS6428099A - Artificial satellite separation system - Google Patents

Artificial satellite separation system

Info

Publication number
JPS6428099A
JPS6428099A JP62184802A JP18480287A JPS6428099A JP S6428099 A JPS6428099 A JP S6428099A JP 62184802 A JP62184802 A JP 62184802A JP 18480287 A JP18480287 A JP 18480287A JP S6428099 A JPS6428099 A JP S6428099A
Authority
JP
Japan
Prior art keywords
satellite
spin
frame axis
spring
position eccentric
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.)
Granted
Application number
JP62184802A
Other languages
Japanese (ja)
Other versions
JP2666285B2 (en
Inventor
Goro Shirako
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.)
NEC Corp
Original Assignee
NEC 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
Application filed by NEC Corp filed Critical NEC Corp
Priority to JP62184802A priority Critical patent/JP2666285B2/en
Publication of JPS6428099A publication Critical patent/JPS6428099A/en
Application granted granted Critical
Publication of JP2666285B2 publication Critical patent/JP2666285B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B64G1/645—Separators
    • 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

Abstract

PURPOSE: To apply a spin around a frame axis to a satellite with a simple structure by providing a satellite extruding spring receptacle at a position eccentric to the center of gravity of the spin satellite, and providing a spring between the satellite and a mother spacecraft. CONSTITUTION: A spring 3 is hooked on a mother spacecraft 2 such as a launch vehicle at one end, and it is hooked on a receptacle 5 provided at a position eccentric to a frame axis 4 passing through the center of gravity of a spin satellite 1 at the other end. When a fixing metal 6 is released and the spin satellite 1 is extruded from the mother spacecraft 2 by the spring 3, it is extruded at the position eccentric to the frame axis 4, it is initially rotated in the direction including the frame axis 4, then it is shifted to a spin around the frame axis 4 by the moment of inertia of the spin satellite 1 as time elapses to become the spin satellite 1. The spin satellite 1 is separated from the mother spacecraft 2, and the required spin can be applied to it with a simple structure.
JP62184802A 1987-07-23 1987-07-23 Satellite separation method Expired - Lifetime JP2666285B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62184802A JP2666285B2 (en) 1987-07-23 1987-07-23 Satellite separation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62184802A JP2666285B2 (en) 1987-07-23 1987-07-23 Satellite separation method

Publications (2)

Publication Number Publication Date
JPS6428099A true JPS6428099A (en) 1989-01-30
JP2666285B2 JP2666285B2 (en) 1997-10-22

Family

ID=16159549

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62184802A Expired - Lifetime JP2666285B2 (en) 1987-07-23 1987-07-23 Satellite separation method

Country Status (1)

Country Link
JP (1) JP2666285B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109515764A (en) * 2018-12-29 2019-03-26 西北工业大学 A kind of flat micro-nano satellite separator of controllable rotating angular speed

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS572560A (en) * 1980-06-06 1982-01-07 Hitachi Ltd High voltage semiconductor device
JPS59134100A (en) * 1983-01-20 1984-08-01 日本電気株式会社 Separator for artificial satellite
JPS63297200A (en) * 1987-05-26 1988-12-05 日本電気株式会社 Artificial satellite separator

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS572560A (en) * 1980-06-06 1982-01-07 Hitachi Ltd High voltage semiconductor device
JPS59134100A (en) * 1983-01-20 1984-08-01 日本電気株式会社 Separator for artificial satellite
JPS63297200A (en) * 1987-05-26 1988-12-05 日本電気株式会社 Artificial satellite separator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109515764A (en) * 2018-12-29 2019-03-26 西北工业大学 A kind of flat micro-nano satellite separator of controllable rotating angular speed
CN109515764B (en) * 2018-12-29 2022-04-15 西北工业大学 Flat plate type micro-nano satellite separation device capable of controlling rotation angular velocity

Also Published As

Publication number Publication date
JP2666285B2 (en) 1997-10-22

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