WO2017134689A3 - Adaptable satellite bus - Google Patents

Adaptable satellite bus 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
Application number
PCT/IN2017/050053
Other languages
French (fr)
Other versions
WO2017134689A2 (en
Inventor
Priyank PUNTAMBEKAR
Original Assignee
Axiom Research Labs Private Limited
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 Limited filed Critical Axiom Research Labs Private Limited
Publication of WO2017134689A2 publication Critical patent/WO2017134689A2/en
Publication of WO2017134689A3 publication Critical patent/WO2017134689A3/en

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
    • B64G1/42—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
    • 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
    • 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)
  • Navigation (AREA)
  • Patch Boards (AREA)

Abstract

An adaptable satellite bus (100, 300) is provided. The adaptable satellite bus (100, 300) includes a plurality of coupling brackets. The adaptable satellite bus (100, 300) further includes a plurality of structural panels (106-116) configured to be coupled to each other via the plurality of coupling brackets (104), wherein at least one structural panel of the plurality of structural panels (106-116) includes mounting provisions (118) for supporting one or more different types of payloads, and one or more structural panels include mounting provisions for one or more supporting sub-systems, and wherein configuration of the mounting provisions (118) for supporting one or more different types of payloads and configuration of the mounting provisions (126) for one or more supporting sub-systems are independent of an intended use of the adaptable satellite bus (100). A method (400) for making the adaptable satellite bus (100) also provided.
PCT/IN2017/050053 2016-02-06 2017-02-06 Adaptable satellite bus WO2017134689A2 (en)

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 (en) 2017-08-10
WO2017134689A3 true WO2017134689A3 (en) 2019-04-25

Family

ID=59499648

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IN2017/050053 WO2017134689A2 (en) 2016-02-06 2017-02-06 Adaptable satellite bus

Country Status (1)

Country Link
WO (1) WO2017134689A2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3587282A1 (en) 2018-06-21 2020-01-01 Airbus Oneweb Satellites SAS Satellite control apparatuses and methods

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 (en) 2017-08-10

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