GB2018211A - Satellite - Google Patents

Satellite

Info

Publication number
GB2018211A
GB2018211A GB7905167A GB7905167A GB2018211A GB 2018211 A GB2018211 A GB 2018211A GB 7905167 A GB7905167 A GB 7905167A GB 7905167 A GB7905167 A GB 7905167A GB 2018211 A GB2018211 A GB 2018211A
Authority
GB
United Kingdom
Prior art keywords
satellite
bars
rods
section
lattice structure
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
GB7905167A
Other versions
GB2018211B (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.)
Dornier System GmbH
Original Assignee
Dornier System GmbH
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 Dornier System GmbH filed Critical Dornier System GmbH
Publication of GB2018211A publication Critical patent/GB2018211A/en
Application granted granted Critical
Publication of GB2018211B publication Critical patent/GB2018211B/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
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • 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
    • B64G1/223—Modular spacecraft systems
    • 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
    • B64G1/642—Clamps, e.g. Marman clamps

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Details Of Aerials (AREA)
  • Radio Relay Systems (AREA)
  • Reinforcement Elements For Buildings (AREA)

Abstract

A satellite has a central, thermally stable lattice structure (1) of rods or bars of carbon fibre reinforced plastics material. At the connecting points (3) of the rods or bars, satellite component modules (6 to 11) are mounted. With this form of construction, satellites for various purposes can be more readily constructed. The lattice structure is supported by an adaptor (12) which permits geometrical transition from a circular cross-section (e.g. of a carrier stage) to the lattice cross-section (55). <IMAGE>
GB7905167A 1978-04-08 1979-02-14 Satellite Expired GB2018211B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2815216A DE2815216C2 (en) 1978-04-08 1978-04-08 Satellite structure

Publications (2)

Publication Number Publication Date
GB2018211A true GB2018211A (en) 1979-10-17
GB2018211B GB2018211B (en) 1982-06-03

Family

ID=6036456

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7905167A Expired GB2018211B (en) 1978-04-08 1979-02-14 Satellite

Country Status (5)

Country Link
CH (1) CH642922A5 (en)
DE (1) DE2815216C2 (en)
FR (1) FR2421799A1 (en)
GB (1) GB2018211B (en)
IT (1) IT7967734A0 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182295A (en) * 1985-10-30 1987-05-13 Rca Corp Spacecraft structure for orbital assembly and servicing
GB2270665A (en) * 1992-09-21 1994-03-23 Gen Electric Spacecraft-to-launch-vehicle transition structure.
EP0849166A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Modular spacecraft architecture
EP0849168A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module
EP0849169A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Functionally independent spacecraft module
EP0849167A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Modular spacecraft development process
JPH10181696A (en) * 1996-12-20 1998-07-07 Trw Inc Space craft device module which can be installed outside
CN112298605A (en) * 2020-09-29 2021-02-02 北京空间飞行器总体设计部 Plate-and-bar type satellite main structure

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4834325A (en) * 1985-03-20 1989-05-30 Space Industries, Inc. Modular spacecraft system
DE3609770A1 (en) * 1986-03-22 1987-10-01 Erno Raumfahrttechnik Gmbh PAYLOAD TRANSPORT AND OPERATING DEVICE FOR SPACE VEHICLES

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2835548A (en) * 1957-08-01 1958-05-20 Robert C Baumann Satellite structure
US3258225A (en) * 1964-03-13 1966-06-28 Fred H Esch Satellite mounting structure
GB1169342A (en) * 1966-01-17 1969-11-05 British Aircraft Corp Ltd Form Improvements in Rocket Powered Aerial and Space Vehicles

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182295A (en) * 1985-10-30 1987-05-13 Rca Corp Spacecraft structure for orbital assembly and servicing
GB2182295B (en) * 1985-10-30 1990-01-31 Rca Corp Spacecraft structure for orbital assembly and servicing
GB2270665A (en) * 1992-09-21 1994-03-23 Gen Electric Spacecraft-to-launch-vehicle transition structure.
FR2695906A1 (en) * 1992-09-21 1994-03-25 Gen Electric Spaceship-launcher association and transition piece for this association.
US5337980A (en) * 1992-09-21 1994-08-16 General Electric Co. Spacecraft-to-launch-vehicle transition
GB2270665B (en) * 1992-09-21 1996-09-18 Gen Electric Spacecraft-to-launch-vehicle transition
EP0849166A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Modular spacecraft architecture
EP0849168A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module
EP0849169A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Functionally independent spacecraft module
EP0849167A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Modular spacecraft development process
JPH10181696A (en) * 1996-12-20 1998-07-07 Trw Inc Space craft device module which can be installed outside
EP0849172A3 (en) * 1996-12-20 1998-07-08 TRW Inc. Externally mountable spacecraft equipment module
US5897080A (en) * 1996-12-20 1999-04-27 Trw Inc. Externally mountable spacecraft equipment module
US5904317A (en) * 1996-12-20 1999-05-18 Trw Inc. Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module
US5931418A (en) * 1996-12-20 1999-08-03 Trw Inc. Functionally independent spacecraft module
US5961076A (en) * 1996-12-20 1999-10-05 Trw Inc. Modular spacecraft development process
US5979833A (en) * 1996-12-20 1999-11-09 Trw Inc. Modular spacecraft architecture
CN112298605A (en) * 2020-09-29 2021-02-02 北京空间飞行器总体设计部 Plate-and-bar type satellite main structure
CN112298605B (en) * 2020-09-29 2022-03-04 北京空间飞行器总体设计部 Plate-and-bar type satellite main structure

Also Published As

Publication number Publication date
FR2421799B1 (en) 1983-05-27
DE2815216C2 (en) 1984-04-26
GB2018211B (en) 1982-06-03
FR2421799A1 (en) 1979-11-02
CH642922A5 (en) 1984-05-15
IT7967734A0 (en) 1979-04-06
DE2815216A1 (en) 1979-10-11

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee