000 03959nam a2200553 i 4500
001 9295049
003 IEEE
005 20220712210034.0
006 m o d
007 cr |n|||||||||
008 210105s2020 nju ob 001 eng d
010 _z 2020024527 (print)
020 _a9781119692706
_qadobe pdf
020 _z1119692725
_qelectronic bk. : oBook
020 _z9781119692720
_qelectronic bk. : oBook
020 _z9781119692713
_qePub
020 _z1119692717
_qePub
020 _z1119692709
_qadobe pdf
020 _z9781119692584
_qcloth
024 7 _a10.1002/9781119692720
_2doi
035 _a(CaBNVSL)mat09295049
035 _a(IDAMS)0b0000648d5cf5c5
040 _aCaBNVSL
_beng
_erda
_cCaBNVSL
_dCaBNVSL
050 0 0 _aTL3035
082 0 0 _a629.46/43
_223
245 0 0 _aCubeSat antenna design /
_cedited by Dr. Nacer Chahat, NASA Jet Propulsion Laboratory/California Institute of Technology, Pasadena, CA.
250 _aFirst edition.
264 1 _aHoboken, New Jersey, USA :
_bWiley-IEEE,
_c2020.
264 2 _a[Piscataqay, New Jersey] :
_bIEEE Xplore,
_c[2020]
300 _a1 PDF.
336 _atext
_2rdacontent
337 _aelectronic
_2isbdmedia
338 _aonline resource
_2rdacarrier
504 _aIncludes bibliographical references.
505 0 _aIntroduction / 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.
506 _aRestricted to subscribers or individual electronic text purchasers.
520 _a"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"--
_cProvided by publisher.
530 _aAlso available in print.
538 _aMode of access: World Wide Web
650 0 _aArtificial satellites
_xRadio antennas
_xDesign and construction.
_99419
650 0 _aMicrospacecraft
_xDesign and construction.
_99420
655 4 _aElectronic books.
_93294
700 1 _aChahat, Nacer,
_eeditor.
_929746
710 2 _aIEEE Xplore (Online Service),
_edistributor.
_929747
710 2 _aWiley,
_epublisher.
_929748
776 0 8 _iPrint version:
_tCubeSat antenna design
_bFirst edition.
_dHoboken, NJ, USA : Wiley-IEEE, 2020.
_z9781119692584
_w(DLC) 2020024526
856 4 2 _3Abstract with links to resource
_uhttps://ieeexplore.ieee.org/xpl/bkabstractplus.jsp?bkn=9295049
942 _cEBK
999 _c74669
_d74669