WO2017134689A3 - Bus de satellite adaptable - Google Patents

Bus de satellite adaptable Download PDF

Info

Publication number
WO2017134689A3
WO2017134689A3 PCT/IN2017/050053 IN2017050053W WO2017134689A3 WO 2017134689 A3 WO2017134689 A3 WO 2017134689A3 IN 2017050053 W IN2017050053 W IN 2017050053W WO 2017134689 A3 WO2017134689 A3 WO 2017134689A3
Authority
WO
WIPO (PCT)
Prior art keywords
adaptable
satellite bus
supporting
mounting provisions
structural panels
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.)
Ceased
Application number
PCT/IN2017/050053
Other languages
English (en)
Other versions
WO2017134689A2 (fr
Inventor
Priyank PUNTAMBEKAR
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.)
Axiom Research Labs Private Ltd
Original Assignee
Axiom Research Labs Private 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 Axiom Research Labs Private Ltd filed Critical Axiom Research Labs Private Ltd
Publication of WO2017134689A2 publication Critical patent/WO2017134689A2/fr
Anticipated expiration legal-status Critical
Publication of WO2017134689A3 publication Critical patent/WO2017134689A3/fr
Ceased 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
    • B64G1/10—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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/428—Power distribution and management
    • 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
    • B64G1/1021—Earth observation satellites

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Patch Boards (AREA)
  • Navigation (AREA)

Abstract

L'invention concerne un bus de satellite adaptable (100, 300). Le bus de satellite adaptable (100, 300) comprend une pluralité de supports d'accouplement. Le bus de satellite adaptable (100, 300) comprend en outre une pluralité de panneaux structuraux (106-116) conçus pour être accouplés les uns aux autres par l'intermédiaire de la pluralité de supports d'accouplement (104), au moins un panneau structural de la pluralité de panneaux structuraux (106-116) comprenant des dispositions de montage (118) pour supporter un ou plusieurs types différents de charges utiles, et un ou plusieurs panneaux structuraux comprenant des dispositions de montage pour un ou plusieurs sous-systèmes de support, et la configuration des dispositions de montage (118) pour supporter un ou plusieurs types différents de charges utiles et la configuration des dispositions de montage (126) pour un ou plusieurs sous-systèmes de support étant indépendantes d'une utilisation prévue du bus de satellite adaptable (100). L'invention concerne également un procédé (400) pour fabriquer le bus de satellite adaptable (100).
PCT/IN2017/050053 2016-02-06 2017-02-06 Bus de satellite adaptable Ceased WO2017134689A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IN201641004296 2016-02-06
IN201641004296 2016-02-06

Publications (2)

Publication Number Publication Date
WO2017134689A2 WO2017134689A2 (fr) 2017-08-10
WO2017134689A3 true WO2017134689A3 (fr) 2019-04-25

Family

ID=59499648

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IN2017/050053 Ceased WO2017134689A2 (fr) 2016-02-06 2017-02-06 Bus de satellite adaptable

Country Status (1)

Country Link
WO (1) WO2017134689A2 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3587282A1 (fr) * 2018-06-21 2020-01-01 Airbus Oneweb Satellites SAS Appareils et procédés de commande de satellite
CN119683011B (zh) * 2024-11-29 2026-01-27 上海卫星工程研究所 适用于多类载荷的通用化卫星构型

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5755406A (en) * 1995-12-22 1998-05-26 Hughes Electronics Modular, independent subsystem design satellite bus and variable communication payload configurations and missions
US6206237B1 (en) * 1999-03-08 2001-03-27 Pepsico, Inc. Bottle dispenser
US20110296675A1 (en) * 2009-08-26 2011-12-08 Roopnarine Means for rapidly assembling a spacecraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5755406A (en) * 1995-12-22 1998-05-26 Hughes Electronics Modular, independent subsystem design satellite bus and variable communication payload configurations and missions
US6206237B1 (en) * 1999-03-08 2001-03-27 Pepsico, Inc. Bottle dispenser
US20110296675A1 (en) * 2009-08-26 2011-12-08 Roopnarine Means for rapidly assembling a spacecraft

Also Published As

Publication number Publication date
WO2017134689A2 (fr) 2017-08-10

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