USD756887S1 - Cubesat with a chipsat deployer - Google Patents
Cubesat with a chipsat deployer Download PDFInfo
- 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
- Authority
- US
- United States
- Prior art keywords
- chipsat
- cubesat
- deployer
- ornamental design
- view
- 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.)
- Active
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Description
Claims (1)
- The ornamental design for a cubesat with a chipsat deployer, as shown and described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/477,297 USD756887S1 (en) | 2013-12-20 | 2013-12-20 | Cubesat with a chipsat deployer |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/477,297 USD756887S1 (en) | 2013-12-20 | 2013-12-20 | Cubesat with a chipsat deployer |
Publications (1)
Publication Number | Publication Date |
---|---|
USD756887S1 true USD756887S1 (en) | 2016-05-24 |
Family
ID=55970142
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29/477,297 Active USD756887S1 (en) | 2013-12-20 | 2013-12-20 | Cubesat with a chipsat deployer |
Country Status (1)
Country | Link |
---|---|
US (1) | USD756887S1 (en) |
Cited By (2)
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)
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 |
-
2013
- 2013-12-20 US US29/477,297 patent/USD756887S1/en active Active
Patent Citations (12)
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)
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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