CubeSat antenna design / edited by Dr. Nacer Chahat, NASA Jet Propulsion Laboratory/California Institute of Technology, Pasadena, CA.
Contributor(s): Chahat, Nacer [editor.]
| IEEE Xplore (Online Service) [distributor.] | Wiley [publisher.].
Material type: 
BookPublisher: Hoboken, New Jersey, USA : Wiley-IEEE, 2020Distributor: [Piscataqay, New Jersey] : IEEE Xplore, [2020]Edition: First edition.Description: 1 PDF.Content type: text Media type: electronic Carrier type: online resourceISBN: 9781119692706.Subject(s): Artificial satellites -- Radio antennas -- Design and construction | Microspacecraft -- Design and constructionGenre/Form: Electronic books.Additional physical formats: Print version:: CubeSat antenna designDDC classification: 629.46/43 Online resources: Abstract with links to resource Also available in print.Includes bibliographical references.
Introduction / Nacer Chahat -- Mars Cube One / Nacer Chahat, Emmanuel Decrossas, M Michael Kobayashi -- Radar in a CubeSat: RainCube / Nacer Chahat, Jonathan Sauder, Alessandra Babuscia, Mark Thomson -- One Meter Reflectarray Antenna: OMERA / Nacer Chahat, Manan Arya, Jonathan Sauder, Ellen Thiel, Min Zhou, Tom Cwik -- X/Ka-Band One Meter Mesh Reflector for 12U-Class CubeSat / Nacer Chahat, Jonathan Sauder, Gregg Freebury -- Inflatable Antenna for CubeSat / Alessandra Babuscia, Jonathan Sauder, Aman Chandra, Jekan Thangavelautham -- High Aperture Efficiency All-Metal Patch Array / Nacer Chahat -- Metasurface Antennas: Flat Antennas for Small Satellites / David GonzA�lez-Ovejero, Okan Yurduseven, Goutam Chattopadhyay, Nacer Chahat.
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"This book surveys a variety of antenna designs used for CubeSat communication and radar by the Jet Propulsion Laboratory (JPL). The first chapter presents a brief introduction of CubeSats. The second chapter illustrates the telecommunication subsystem of Mars Cube One (MarCO) mission, with an emphasis on the antenna development. The third chapter describes the enabling technology of Radar in a CubeSat (RainCube): the 0.5m deployable mesh reflector. Chapter 4 presents the electrical and mechanical design of the largest reflectarray compatible with a 6U-class CubeSat: OMERA (one meter reflectarray antenna). Chapter 5 explains the development of a one-meter mesh reflector for telecommunication at X- and Ka-band for deep space missions. In Chapter 6, an inflatable antenna operating at X-band is shown from an electrical and mechanical point of view with all the challenges associated with operation in space. In Chapter 7, depicts how a novel patch array mainly made of metal is used on a CubeSat. Finally, Chapter 8 describes the design of multiple metasurface antennas"-- Provided by publisher.
Also available in print.
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