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In-Space Deployable Reflectarray Antenna: Current and FutureTechnologies associated with a 10-m X/Ka-band dual-frequency reflectarray antenna have been developed for deep space communication applications. The first task is the development of a 3-m diameter X/Ka dual frequency reflectarray which serves as a stepping-stone to the 10-m aperture antenna. The second task is to develop a deployable frame.
Document ID
20150014723
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/45354
Authors
Fang, Houfei (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Knarr, Kevin (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Quijano, Ubaldo (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Huang, John (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Thomson, Mark (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2015
Publication Date
April 7, 2008
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Meeting Information
Meeting: AIAA Gossamer Spacecraft Forum
Location: Schaumburg, IL
Country: United States
Start Date: April 7, 2008
End Date: April 10, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other

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