Paper
7 October 2014 Orbital checkout result of the dual-frequency precipitation radar on the global precipitation measurement core spacecraft
K. Furukawa, M. Kojima, T. Miura, Y. Hyakusoku, H. Kai, T. Ishikiri, T. Iguchi, H. Hanado, K. Nakagawa, M. Okumura
Author Affiliations +
Abstract
The Dual-frequency Precipitation Radar (DPR) on the Global Precipitation Measurement (GPM) core satellite was developed by Japan Aerospace Exploration Agency (JAXA) and National Institute of Information and Communications Technology (NICT). The GPM is a follow-on mission of the Tropical Rainfall Measuring Mission (TRMM). The objectives of the GPM mission are to observe global precipitation more frequently and accurately than TRMM. The frequent precipitation measurement about every three hours will be achieved by some constellation satellites with microwave radiometers (MWRs) or microwave sounders (MWSs), which will be developed by various countries. The accurate measurement of precipitation in mid-high latitudes will be achieved by the DPR. The GPM core satellite is a joint product of National Aeronautics and Space Administration (NASA), JAXA and NICT. NASA developed the satellite bus and the GPM Microwave Imager (GMI), and JAXA and NICT developed the DPR. JAXA and NICT developed the DPR through procurement. The contract for DPR was awarded to NEC TOSHIBA Space Systems, Ltd. The configuration of precipitation measurement using active radar and a passive radiometer is similar to TRMM. The major difference is that DPR is used in GPM instead of the precipitation radar (PR) in TRMM. The inclination of the core satellite is 65 degrees, and the flight altitude is about 407 km. The non-sun-synchronous circular orbit is necessary for measuring the diurnal change of rainfall similarly to TRMM. The DPR consists of two radars, which are Ku-band (13.6 GHz) precipitation radar (KuPR) and Ka-band (35.5 GHz) precipitation radar (KaPR). Both KuPR and KaPR have almost the same design as TRMM PR. The DPR system design and performance were verified through the development test and the proto flight test. DPR had handed over to NASA and integration of the DPR to the GPM core spacecraft had completed in May 2012. GPM core spacecraft satellite system test had completed in November 2013. The result of the satellite system test concerning to the DPR satisfied system requirements. GPM core observatory was shipped to Tanegashima Space Center, JAPAN and Launch Site Operations had started on November 2013 and GPM core observatory was launched at 18:37:00 (UT) on February 27, 2014 successfully. DPR orbital check out was completed in May 2014. The orbital check out and the initial calibration and validation operation result of DPR is reported.
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K. Furukawa, M. Kojima, T. Miura, Y. Hyakusoku, H. Kai, T. Ishikiri, T. Iguchi, H. Hanado, K. Nakagawa, and M. Okumura "Orbital checkout result of the dual-frequency precipitation radar on the global precipitation measurement core spacecraft", Proc. SPIE 9241, Sensors, Systems, and Next-Generation Satellites XVIII, 92410S (7 October 2014); https://doi.org/10.1117/12.2067114
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KEYWORDS
Radar

Space operations

Satellites

Calibration

Microwave radiation

Observatories

Antennas

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