USD756887S1 - Cubesat with a chipsat deployer - Google Patents

Cubesat with a chipsat deployer Download PDF

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Publication number
USD756887S1
USD756887S1 US29/477,297 US201329477297F USD756887S US D756887 S1 USD756887 S1 US D756887S1 US 201329477297 F US201329477297 F US 201329477297F US D756887 S USD756887 S US D756887S
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United States
Prior art keywords
chipsat
cubesat
deployer
ornamental design
view
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US29/477,297
Inventor
Andrew Simon Filo
Matthew Frederick Reyes
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Individual
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Individual
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Priority to US29/477,297 priority Critical patent/USD756887S1/en
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Description

FIG. 1 is an isometric view of the cubesat with a chipsat deployer showing our new design;
FIG. 2 is a side view thereof; and,
FIG. 3 is a top view thereof.
FIG. 3 is shown at a larger scale than FIG. 2 is shown. The broken lines in the figures are for the purpose of illustrating portions of the cubesat with a chipsat deployer and form no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for a cubesat with a chipsat deployer, as shown and described.
US29/477,297 2013-12-20 2013-12-20 Cubesat with a chipsat deployer Active USD756887S1 (en)

Priority Applications (1)

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US29/477,297 USD756887S1 (en) 2013-12-20 2013-12-20 Cubesat with a chipsat deployer

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US29/477,297 USD756887S1 (en) 2013-12-20 2013-12-20 Cubesat with a chipsat deployer

Publications (1)

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USD756887S1 true USD756887S1 (en) 2016-05-24

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US29/477,297 Active USD756887S1 (en) 2013-12-20 2013-12-20 Cubesat with a chipsat deployer

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160197394A1 (en) * 2013-09-06 2016-07-07 MMA Design, LLC Deployable Reflectarray Antenna Structure
CN110562495B (en) * 2019-08-15 2021-04-13 南京理工大学 Cube star offset momentum attitude control system

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4537838A (en) * 1982-07-05 1985-08-27 Hartag Ag System with several panels containing photoelectric elements for the production of electric current
US4664343A (en) * 1984-08-29 1987-05-12 Scott Science & Technology, Inc. Satelite transfer vehicle
US4834325A (en) * 1985-03-20 1989-05-30 Space Industries, Inc. Modular spacecraft system
US4936528A (en) * 1988-05-11 1990-06-26 General Research Corporation Method and apparatus for orbital debris mitigation
US5271582A (en) * 1990-06-29 1993-12-21 Standard Space Platforms Corp. Modular mother satellite bus for subsidiary payloads
US5511748A (en) * 1993-11-12 1996-04-30 Scott; David R. Method for extending the useful life of a space satellite
US6017002A (en) * 1997-07-21 2000-01-25 Hughes Electronics Corporation Thin-film solar reflectors deployable from an edge-stowed configuration
US6284966B1 (en) * 2000-03-06 2001-09-04 The Aerospace Corporation Power sphere nanosatellite
US20060284006A1 (en) * 2005-04-25 2006-12-21 Chasman Daniel B Missile control system and method
US20080143636A1 (en) * 2005-03-04 2008-06-19 Eads Astrium Limited Phased Array Antenna
US8511615B2 (en) * 2010-12-23 2013-08-20 Thales Deployable structure forming an antenna equipped with a solar generator for a satellite
US20140263844A1 (en) * 2013-03-15 2014-09-18 The Boeing Company Component Deployment System

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4537838A (en) * 1982-07-05 1985-08-27 Hartag Ag System with several panels containing photoelectric elements for the production of electric current
US4664343A (en) * 1984-08-29 1987-05-12 Scott Science & Technology, Inc. Satelite transfer vehicle
US4834325A (en) * 1985-03-20 1989-05-30 Space Industries, Inc. Modular spacecraft system
US4936528A (en) * 1988-05-11 1990-06-26 General Research Corporation Method and apparatus for orbital debris mitigation
US5271582A (en) * 1990-06-29 1993-12-21 Standard Space Platforms Corp. Modular mother satellite bus for subsidiary payloads
US5511748A (en) * 1993-11-12 1996-04-30 Scott; David R. Method for extending the useful life of a space satellite
US6017002A (en) * 1997-07-21 2000-01-25 Hughes Electronics Corporation Thin-film solar reflectors deployable from an edge-stowed configuration
US6284966B1 (en) * 2000-03-06 2001-09-04 The Aerospace Corporation Power sphere nanosatellite
US20080143636A1 (en) * 2005-03-04 2008-06-19 Eads Astrium Limited Phased Array Antenna
US20060284006A1 (en) * 2005-04-25 2006-12-21 Chasman Daniel B Missile control system and method
US8511615B2 (en) * 2010-12-23 2013-08-20 Thales Deployable structure forming an antenna equipped with a solar generator for a satellite
US20140263844A1 (en) * 2013-03-15 2014-09-18 The Boeing Company Component Deployment System

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160197394A1 (en) * 2013-09-06 2016-07-07 MMA Design, LLC Deployable Reflectarray Antenna Structure
US10263316B2 (en) * 2013-09-06 2019-04-16 MMA Design, LLC Deployable reflectarray antenna structure
US10763569B2 (en) 2013-09-06 2020-09-01 M.M.A. Design, LLC Deployable reflectarray antenna structure
US10826157B2 (en) 2013-09-06 2020-11-03 MMA Design, LLC Deployable reflectarray antenna structure
US11901605B2 (en) 2013-09-06 2024-02-13 M.M.A. Design, LLC Deployable antenna structure
CN110562495B (en) * 2019-08-15 2021-04-13 南京理工大学 Cube star offset momentum attitude control system

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