ISS_RapidScat
type: Concept
change note: 2021-07-02 12:43:12.0 [sritz] Insert Concept add broader relation (ISS_RapidScat [60573ec9-34ea-4602-b865-5b8a9fd3c8fb,663809] - G - I [af0968ce-ffe3-44a0-86de-2ec9b9a8fa5d,658129]);
change note: 2021-07-02 12:46:21.0 [sritz] insert WeightedRelation (id: null related concept uuid: 93c5d18c-be62-46c4-9545-42f73a854d85 relationship type: null relationship value: null generated by: null);
change note: 2021-07-02 12:43:44.0 [sritz] insert AltLabel (id: null category: primary text: International Space Station Rapid Scatterometer language code: en);
change note: 2021-07-02 12:44:31.0 [sritz] insert Definition (id: null text: The InternISS-RapidScat ational Space Station Rapid Scatterometer (ISS-RapidScat) mission was launched on 20 September 2014 from the Cape Canaveral Air Force Station in Florida with the primary goal of measuring ocean surface wind vectors, calibrated to a 10 meter reference height, as a continuation of the QuikSCAT climate data record, and as a demonstration of the ability to cost-effectively re-use existing hardware, originally designed and manufactured for test purposes, as an operational space flight Earth remote sensing mission in support of fundamental scientific research of Earth's weather, oceans, and coupled climate system. After successfully being mounted and properly calibrated on the ISS, the RapidScat instrument began providing its first set of calibrated, science-quality measurements on 3 October 2014. As a bi-product of the low inclination orbit of ISS, RapidScat is in a unique position to provide measurements that are asynchronous with respect to the solar day cycle of the Earths; this translates to RapidScat having the unique capability (in contrast to all other past and present space-borne scatterometers) of observing diurnal and semi-diurnal variability over seasonal time scales. The ISS-RapidScat mission is particularly blessed to have contemporaneous measurements from QuikSCAT (albeit limited due to QuikSCAT's fixed antenna position) as a way to ensure consistently calibrated measurements to ensure accurate observation and continued study of the coupled Earth climate system. The PO.DAAC functions as the primary archive and distribution center for the RapidScat data produced directly by the ISS-RapidScat Science Data Systems (SDS) team at JPL. language code: en);
in scheme: projects
definition: The InternISS-RapidScat ational Space Station Rapid Scatterometer (ISS-RapidScat) mission was launched on 20 September 2014 from the Cape Canaveral Air Force Station in Florida with the primary goal of measuring ocean surface wind vectors, calibrated to a 10 meter reference height, as a continuation of the QuikSCAT climate data record, and as a demonstration of the ability to cost-effectively re-use existing hardware, originally designed and manufactured for test purposes, as an operational space flight Earth remote sensing mission in support of fundamental scientific research of Earth's weather, oceans, and coupled climate system. After successfully being mounted and properly calibrated on the ISS, the RapidScat instrument began providing its first set of calibrated, science-quality measurements on 3 October 2014. As a bi-product of the low inclination orbit of ISS, RapidScat is in a unique position to provide measurements that are asynchronous with respect to the solar day cycle of the Earths; this translates to RapidScat having the unique capability (in contrast to all other past and present space-borne scatterometers) of observing diurnal and semi-diurnal variability over seasonal time scales. The ISS-RapidScat mission is particularly blessed to have contemporaneous measurements from QuikSCAT (albeit limited due to QuikSCAT's fixed antenna position) as a way to ensure consistently calibrated measurements to ensure accurate observation and continued study of the coupled Earth climate system. The PO.DAAC functions as the primary archive and distribution center for the RapidScat data produced directly by the ISS-RapidScat Science Data Systems (SDS) team at JPL.

G - I
type: Concept