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WO2017134686A3 - System and method for interfacing a payload with an onboard device in a spacecraft - Google Patents

System and method for interfacing a payload with an onboard device in a spacecraft Download PDF

Info

Publication number
WO2017134686A3
WO2017134686A3 PCT/IN2017/050050 IN2017050050W WO2017134686A3 WO 2017134686 A3 WO2017134686 A3 WO 2017134686A3 IN 2017050050 W IN2017050050 W IN 2017050050W WO 2017134686 A3 WO2017134686 A3 WO 2017134686A3
Authority
WO
WIPO (PCT)
Prior art keywords
payload
spacecraft
onboard device
interfacing
system includes
Prior art date
Application number
PCT/IN2017/050050
Other languages
French (fr)
Other versions
WO2017134686A2 (en
Inventor
Nirmal GADDE
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 WO2017134686A2 publication Critical patent/WO2017134686A2/en
Publication of WO2017134686A3 publication Critical patent/WO2017134686A3/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)
  • Connection Of Plates (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

A system for interfacing at least one payload with at least one onboard device in a spacecraft is presented. The system includes a detachable bracket having a base and at least one slot, and configured to receive the at least one payload. Also, a design of the at least one payload is independent of a design of the spacecraft. Further, the system includes at least one adapter disposed within the at least one slot and configured to communicatively couple the at least one payload to the at least one onboard device in the spacecraft. In addition, the system includes a plurality of fasteners operatively coupled to the detachable bracket and configured to fasten the at least one payload to the base of the detachable bracket.
PCT/IN2017/050050 2016-02-06 2017-02-03 System and method for interfacing a payload with an onboard device in a spacecraft WO2017134686A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IN201641004294 2016-02-06
IN201641004294 2016-02-06

Publications (2)

Publication Number Publication Date
WO2017134686A2 WO2017134686A2 (en) 2017-08-10
WO2017134686A3 true WO2017134686A3 (en) 2019-01-17

Family

ID=59499587

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IN2017/050050 WO2017134686A2 (en) 2016-02-06 2017-02-03 System and method for interfacing a payload with an onboard device in a spacecraft

Country Status (1)

Country Link
WO (1) WO2017134686A2 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4880187A (en) * 1986-01-16 1989-11-14 Trw Inc. Multipurpose modular spacecraft
US6543724B1 (en) * 1999-07-22 2003-04-08 Lockheed Martin Corporation Miniature satellite design
US20040245399A1 (en) * 2002-07-23 2004-12-09 Blackwell-Thompson Judith C. System and methods for integrating a payload with a launch vehicle
US7042710B1 (en) * 2003-06-10 2006-05-09 Garmin Ltd. Mounting system for electronic components
US20150210392A1 (en) * 2014-01-24 2015-07-30 L-3 Communications Integrated Systems L.P. Reconfigurable Payload Systems (RPS) With Operational Load Envelopes For Aircraft And Methods Related Thereto

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4880187A (en) * 1986-01-16 1989-11-14 Trw Inc. Multipurpose modular spacecraft
US6543724B1 (en) * 1999-07-22 2003-04-08 Lockheed Martin Corporation Miniature satellite design
US20040245399A1 (en) * 2002-07-23 2004-12-09 Blackwell-Thompson Judith C. System and methods for integrating a payload with a launch vehicle
US7042710B1 (en) * 2003-06-10 2006-05-09 Garmin Ltd. Mounting system for electronic components
US20150210392A1 (en) * 2014-01-24 2015-07-30 L-3 Communications Integrated Systems L.P. Reconfigurable Payload Systems (RPS) With Operational Load Envelopes For Aircraft And Methods Related Thereto

Also Published As

Publication number Publication date
WO2017134686A2 (en) 2017-08-10

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