IGARSS 2018 - 2018 IEEE International Geoscience and Remote Sensing Symposium 2018
DOI: 10.1109/igarss.2018.8519194
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The Radar-in-a-Cubesat (RAINCUBE) and Measurement Results

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Cited by 16 publications
(6 citation statements)
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“…RainCube (Radar in a CubeSat) is a 6U CubeSat mission developed between the Jet Propulsion Laboratory (JPL) and Tyvak Nano-Satellite Systems (Tyvak), which is the first ever radar instrument in a CubeSat. [1][2][3][4] The objective of the mission is to develop, launch, and operate a 35.75-GHz nadir-pointing precipitation profiling radar payload to validate a new miniaturized architecture for Ka-band atmospheric radars and an ultracompact deployable Ka-band antenna design in the space environment, which are compatible with a 6U CubeSat platform. Through a competitive bid process, the RainCube JPL team selected Tyvak Nanosatellite Systems, LLC in Irvine, California, to develop the flight system, integrate the payload, and operate the payload on orbit.…”
Section: Introductionmentioning
confidence: 99%
“…RainCube (Radar in a CubeSat) is a 6U CubeSat mission developed between the Jet Propulsion Laboratory (JPL) and Tyvak Nano-Satellite Systems (Tyvak), which is the first ever radar instrument in a CubeSat. [1][2][3][4] The objective of the mission is to develop, launch, and operate a 35.75-GHz nadir-pointing precipitation profiling radar payload to validate a new miniaturized architecture for Ka-band atmospheric radars and an ultracompact deployable Ka-band antenna design in the space environment, which are compatible with a 6U CubeSat platform. Through a competitive bid process, the RainCube JPL team selected Tyvak Nanosatellite Systems, LLC in Irvine, California, to develop the flight system, integrate the payload, and operate the payload on orbit.…”
Section: Introductionmentioning
confidence: 99%
“…This design achieves high radar sensitivity, while significantly reducing the overall size, weight, and power consumption (SWaP) of the instrument. This approach follows that of RainCube, a Ka-band spaceborne precipitation radar in a CubeSat developed previously by JPL (Beauchamp et al, 2017;Peral et al, 2018a;Peral et al, 2018b). The G-band radar, in a prototype stage, was operated on frequency modulated continuous wave (FMCW) mode during this deployment to eliminate the blind range and improve the sensitivity, and included Doppler capability to complement the multifrequency measurements.…”
Section: Cloudcube Instrumentmentioning
confidence: 99%
“…Hence, bandwidth-efficient communication systems with high data rates are required for reliable delivery of the information; thereby reducing the number of passes required. For example, the CubeSat for precipitation monitoring in [106] generates a daily payload of 1.73 Gb, while the available data rate is 50 kbps. Also, the spacecraft has a transmission duty cycle of only 25%, in order to be compliant with the power limitation.…”
Section: Modulation and Codingmentioning
confidence: 99%