GB2002307A - Space spin up and ejection apparatus - Google Patents

Space spin up and ejection apparatus

Info

Publication number
GB2002307A
GB2002307A GB7831710A GB7831710A GB2002307A GB 2002307 A GB2002307 A GB 2002307A GB 7831710 A GB7831710 A GB 7831710A GB 7831710 A GB7831710 A GB 7831710A GB 2002307 A GB2002307 A GB 2002307A
Authority
GB
United Kingdom
Prior art keywords
payload
ejection apparatus
space
spin
space spin
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
GB7831710A
Other versions
GB2002307B (en
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.)
British Aircraft Corp Ltd
Original Assignee
British Aircraft Corp 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 British Aircraft Corp Ltd filed Critical British Aircraft Corp Ltd
Priority to GB7831710A priority Critical patent/GB2002307B/en
Publication of GB2002307A publication Critical patent/GB2002307A/en
Application granted granted Critical
Publication of GB2002307B publication Critical patent/GB2002307B/en
Expired legal-status Critical Current

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
    • B64G1/6459Fluid-actuated
    • 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
    • B64G1/642Clamps, e.g. Marman clamps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/002Launch systems
    • 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
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281Spin-stabilised spacecraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radio Relay Systems (AREA)

Abstract

Apparatus for launching a payload 34 (for example, a satellite) from a carrier spacecraft 30 (for example, a space shuttle vehicle) in space arranged to urge the payload away from the carrier spacecraft and also to spin the payload up to a desired spin rate. The apparatus is also arranged to re-accept a payload after launch. <IMAGE>
GB7831710A 1977-08-03 1978-07-31 Spacecraft spin up and ejection apparatus Expired GB2002307B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7831710A GB2002307B (en) 1977-08-03 1978-07-31 Spacecraft spin up and ejection apparatus

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3248777 1977-08-03
GB7831710A GB2002307B (en) 1977-08-03 1978-07-31 Spacecraft spin up and ejection apparatus

Publications (2)

Publication Number Publication Date
GB2002307A true GB2002307A (en) 1979-02-21
GB2002307B GB2002307B (en) 1982-01-13

Family

ID=26261397

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7831710A Expired GB2002307B (en) 1977-08-03 1978-07-31 Spacecraft spin up and ejection apparatus

Country Status (1)

Country Link
GB (1) GB2002307B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0006126A1 (en) * 1978-05-30 1980-01-09 Hughes Aircraft Company Spin activated safety circuit for spacecraft
FR2449595A1 (en) * 1979-02-21 1980-09-19 Spar Aerospace Ltd FINAL CONTROL DEVICE FOR SATELLITE
US5040748A (en) * 1990-02-20 1991-08-20 General Dynamics Corporation/Space Systems Division Payload adapter ring
GB2385310A (en) * 2002-02-14 2003-08-20 Insys Ltd Satellite launch assembly including means for connection and release

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0006126A1 (en) * 1978-05-30 1980-01-09 Hughes Aircraft Company Spin activated safety circuit for spacecraft
FR2449595A1 (en) * 1979-02-21 1980-09-19 Spar Aerospace Ltd FINAL CONTROL DEVICE FOR SATELLITE
US5040748A (en) * 1990-02-20 1991-08-20 General Dynamics Corporation/Space Systems Division Payload adapter ring
GB2385310A (en) * 2002-02-14 2003-08-20 Insys Ltd Satellite launch assembly including means for connection and release

Also Published As

Publication number Publication date
GB2002307B (en) 1982-01-13

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee