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20240529224311.1 |
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|a 9781119692713
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|a 1119692717
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|a (OCoLC)ebc1227389067
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|d EBLCP
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|a GWRE
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|a TL3035
|b .C434 2020
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|a Chahat, Nacer.
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|a CubeSat Antenna Design
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| 260 |
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|a Newark :
|b John Wiley & Sons, Incorporated,
|c 2020.
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| 300 |
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|a 1 online resource (355 p.)
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|a text
|b txt
|2 rdacontent.
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|a computer
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|2 rdamedia.
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|a online resource
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|a JPL Space Science and Technology Ser.
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|a Description based upon print version of record.
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|a Cover -- Title Page -- Copyright -- Contents -- Preface -- Editor Biography -- Notes on Contributors -- Chapter 1 Introduction -- 1.1 Description of CubeSats -- 1.1.1 Introduction -- 1.1.2 Form Factors -- 1.1.3 Brief Introduction to CubeSat Subsystems -- 1.1.4 CubeSat Antennas -- 1.1.5 Effect of Space Environment on Antennas -- 1.2 Conclusion -- 1.2 Acknowledgments -- 1.2 References -- Chapter 2 Mars Cube One -- 2.1 Mission Description -- 2.2 Iris Radio -- 2.3 X-Band Subsystem -- 2.3.1 Frequency Allocation -- 2.3.2 Near Earth Communications Using Low Gain Antennas.
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|a 2.3.3 Mars-to-Earth Communications -- 2.4 Entry, Descent, and Landing UHF Link -- 2.4.1 State-of-the-Art of UHF Deployable CubeSat Antennas -- 2.4.2 Circularly Polarized Loop Antenna Concept -- 2.4.3 Mechanical Configuration and Deployment Scheme -- 2.4.4 Simulations and Measurements -- 2.4.5 In-Flight Performance -- 2.5 Conclusions -- 2.5 Acknowledgments -- 2.5 References -- Chapter 3 Radar in a CubeSat: RainCube -- 3.1 Mission Description -- 3.2 Deployable High-Gain Antenna -- 3.2.1 State of the Art -- 3.2.2 Parabolic Reflector Antenna Design -- 3.2.3 RainCube High-Gain Antenna.
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|a 3.2.4 Mechanical Deployment -- 3.2.5 Design and Testing for the Space Environment -- 3.2.6 In-Flight Performance -- 3.3 Telecommunication Challenge -- 3.4 Conclusion -- 3.4 Acknowledgments -- 3.4 References -- Chapter 4 One Meter Reflectarray Antenna: OMERA -- 4.1 Introduction -- 4.2 Reflectarray Antennas -- 4.2.1 Introductions to Reflectarray -- 4.2.2 Advantages of Reflectarray -- 4.2.3 Drawbacks of Reflectarray -- 4.2.4 State of the Art -- 4.3 OMERA -- 4.3.1 Antenna Description -- 4.3.2 Deployable Feed -- 4.3.3 Reflectarray Design -- 4.3.4 Deployment Accuracy -- 4.3.5 Effect of Struts.
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|a 4.3.6 Predicted Gain and Efficiency -- 4.3.7 Prototype and Measurements -- 4.4 Conclusion -- 4.4 Acknowledgments -- 4.4 References -- Chapter 5 X/Ka-Band One Meter Mesh Reflector for 12U-Class CubeSat -- 5.1 Introduction -- 5.2 Mechanical Design -- 5.2.1 Trade Studies -- 5.2.2 Structural Design of the Reflector -- 5.2.3 Deployment -- 5.3 X/Ka RF Design -- 5.3.1 Antenna Configuration and Simulation Model -- 5.3.2 X-Band Feed and Mesh Reflector -- 5.3.3 Ka-Band Mesh Reflector -- 5.3.4 X/Ka-band Mesh Reflector -- 5.4 Conclusion -- 5.4 Acknowledgments -- 5.4 References.
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|a Chapter 6 Inflatable Antenna for CubeSat -- 6.1 Introduction -- 6.2 Inflatable High Gain Antenna -- 6.2.1 State of the Art -- 6.2.2 Inflatable Antenna Design at X-Band -- 6.2.3 Structural Design -- 6.2.4 Inflation and On-Orbit Rigidization -- 6.3 Spacecraft Design Challenges -- 6.4 Conclusion -- 6.4 Acknowledgments -- 6.4 References -- Chapter 7 High Aperture Efficiency All-Metal Patch Array -- 7.1 Introduction -- 7.2 State of the Art -- 7.3 Dual-Band Circularly Polarized 8 × 8 Patch Array -- 7.3.1 Requirements -- 7.3.2 Unit Cell Optimization -- 7.3.3 8 × 8 Patch Array.
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|a 7.3.4 Comparison With State-of-the-Art.
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| 776 |
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|i Print version:
|a Chahat, Nacer
|t CubeSat Antenna Design
|d Newark : John Wiley & Sons, Incorporated,c2020
|z 9781119692584.
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| 830 |
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0 |
|a JPL Space Science and Technology Ser.
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| 856 |
4 |
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|u http://ebookcentral.proquest.com/lib/ucb/detail.action?docID=6424571
|z Full Text (via ProQuest)
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|a .b117419874
|b 05-18-21
|c 03-02-21
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|d Online
|e TL3035 .C434 2020
|h Library of Congress classification
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