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Ultra-Compact Ka-Band Parabolic Deployable Antenna for RADAR and Interplanetary CubeSatsOver the past several years, technology and launch opportunities for CubeSats have exploded, enabling a wide variety of missions. However, as instruments become more complex and CubeSats travel deeper into space, data communication rates become an issue. To solve this challenge, JPL has initiated a research and technology development effort to design a 0.5 meter Ka-band parabolic deployable antenna (KaPDA) which would stow in 1.5U (10 x 10 x 15 cu cm) and provide 42dB of gain (50% efficiency). A folding rib architecture and dual reflector Cassegrainian design was selected as it best balances RF gain and stowed size. The design implements an innovative telescoping waveguide and gas powered deployment. RF simulations show that after losses, the antenna would have over 42 dB gain, supported by preliminary test results. KaPDA would create opportunities for a host of new CubeSat missions by allowing high data rate communication which would enable using high fidelity instruments or venturing further into deep space, including potential interplanetary missions. Additionally KaPDA would provide a solution for other small antenna needs and the opportunity to obtain Earth science data. This paper discusses the design challenges encountered, the architecture of the solution, and the antennas expected performance capabilities.
Document ID
20170008200
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Sauder, Jonathan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chahat, Nacer
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Thomson, Mark
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hodges, Richard
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Peral, Eva
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rahmat-Samii, Yahya
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 1, 2017
Publication Date
August 8, 2015
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Communications And Radar
Report/Patent Number
SSC15-VI-7
Meeting Information
Meeting: Annual AIAA/USU Conference on Small Satellites
Location: Logan, UT
Country: United States
Start Date: August 8, 2015
End Date: August 13, 2015
Sponsors: Utah State Univ., American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other

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