The SMAP Spacecraft and Antenna |
[SatNews]
Scheduled for launch on January 29, 2015, NASA's Soil Moisture Active Passive (SMAP) instrument will measure the moisture lodged in Earth's soils with an unprecedented accuracy and resolution. The instrument's three main parts are a radar, a radiometer and the largest rotating mesh antenna ever deployed in space.
SMAP : Mission Description
Objectives: SMAP will provide global measurements of soil moisture and its freeze/thaw state. These measurements will be used to enhance understanding of processes that link the water, energy and carbon cycles, and to extend the capabilities of weather and climate prediction models. SMAP data will also be used to quantify net carbon flux in boreal landscapes and to develop improved flood prediction and drought monitoring capabilities. >> science
Observatory: The SMAP observatory employs a dedicated spacecraft with an instrument suite that will be launched on an expendable launch vehicle into a 680-km near-polar, sun-synchronous orbit, with equator crossings at 6 am and 6 pm local time.
Instrument: The SMAP instrument includes a radiometer and a synthetic aperture radar operating at L-band (1.20-1.41 GHz). The instrument is designed to make coincident measurements of surface emission and backscatter, with the ability to sense the soil conditions through moderate vegetation cover. The instrument measurements will be analyzed to yield estimates of soil moisture and freeze/thaw state. The measurement swath width is 1000 km, providing global coverage within 3 days at the equator and 2 days at boreal latitudes (>45 degrees N). >> more
SMAP : Instrument Specifications
Radar
- Frequency: 1.26 GHz
- Polarizations: VV, HH, HV (not fully polarimetric)
- Relative accuracy (3 km grid): 1 dB (HH and VV), 1.5 dB (HV)
- Data acquisition:
- High-resolution (SAR) data acquired over land
- Low-resolution data acquired globally
Radiometer
- Frequency: 1.41 GHz
- Polarizations: H, V, 3rd & 4th Stokes
- Relative accuracy (30 km grid): 1.3 K
- Data collection:
- High-rate (sub-band) data acquired over land
- Low-rate data acquired globally
Antenna
- Conically-scanning deployable mesh reflector shared by radar and radiometer
- Diameter: 6 meters
- Rotation rate: 14.6 RPM
- Beam efficiency: ~90%
- Spatial Resolution:
- Radiometer (IFOV): 39 km x 47 km
- SAR: 1-3 km (over outer 70% of swath)
- Swath width: 1000 km
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