JPS5383300A - Device for separating artificial satellites - Google Patents

Device for separating artificial satellites

Info

Publication number
JPS5383300A
JPS5383300A JP15829376A JP15829376A JPS5383300A JP S5383300 A JPS5383300 A JP S5383300A JP 15829376 A JP15829376 A JP 15829376A JP 15829376 A JP15829376 A JP 15829376A JP S5383300 A JPS5383300 A JP S5383300A
Authority
JP
Japan
Prior art keywords
satellite
artificial satellites
separating artificial
separating
separate
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
JP15829376A
Other languages
Japanese (ja)
Other versions
JPS5939360B2 (en
Inventor
Kiyoshi Yoshimoto
Hideo Ono
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
Nippon Electric Co Ltd
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, Nippon Electric Co Ltd filed Critical NEC Corp
Priority to JP51158293A priority Critical patent/JPS5939360B2/en
Publication of JPS5383300A publication Critical patent/JPS5383300A/en
Publication of JPS5939360B2 publication Critical patent/JPS5939360B2/en
Expired 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
    • B64G1/641—Interstage or payload connectors
    • 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
    • B64G1/643—Interstage or payload connectors for arranging multiple satellites in a single launcher
    • 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
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1085—Swarms and constellations

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PURPOSE: To provide a device for separating artificial satellite, which can easily and simply separate the satellite by engaging the connector of the satellite with spiral guide and imparting rotary motion and rectilinear motion toward rotary shaft direction to the satellite to separate the satellite.
COPYRIGHT: (C)1978,JPO&Japio
JP51158293A 1976-12-28 1976-12-28 Satellite separation device Expired JPS5939360B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP51158293A JPS5939360B2 (en) 1976-12-28 1976-12-28 Satellite separation device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP51158293A JPS5939360B2 (en) 1976-12-28 1976-12-28 Satellite separation device

Publications (2)

Publication Number Publication Date
JPS5383300A true JPS5383300A (en) 1978-07-22
JPS5939360B2 JPS5939360B2 (en) 1984-09-22

Family

ID=15668431

Family Applications (1)

Application Number Title Priority Date Filing Date
JP51158293A Expired JPS5939360B2 (en) 1976-12-28 1976-12-28 Satellite separation device

Country Status (1)

Country Link
JP (1) JPS5939360B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2564734A (en) * 2017-10-18 2019-01-23 Ellinghaus Frank Panelsat and panelsat launch system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2564734A (en) * 2017-10-18 2019-01-23 Ellinghaus Frank Panelsat and panelsat launch system
GB2564734B (en) * 2017-10-18 2019-07-10 Ellinghaus Frank Panelsat, an agile satellite with fuel free attitude control

Also Published As

Publication number Publication date
JPS5939360B2 (en) 1984-09-22

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