Title :
The HYDROS mission: requirements and system design
Author :
Njoku, Eni ; Spencer, Michael ; McDonald, Kyle ; Smith, Joel ; Houser, Paul ; Doiron, Terence ; O´Neill, Peggy ; Girard, Ralph ; Entekhabi, Dara
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Abstract :
The HYDROS mission is under development by NASA as part of its Earth System Science Pathfinder (ESSP) program. HYDROS is designed to provide global maps of the Earth´s soil moisture and freeze/thaw state every 2-3 days, for weather and climate prediction, water, energy and carbon cycle studies, natural hazards monitoring, and national security applications. HYDROS uses a unique active and passive L-band microwave system that optimizes measurement accuracy, spatial resolution, and coverage. It provides measurements in nearly all weather conditions, regardless of solar illumination. The design of the radar and radiometer electronics, antenna feed system, reflector and science data system, are driven by specific mission and science objectives. These objectives impose requirements on the frequencies, polarizations, sampling, spatial resolution, and accuracy of the system. We describe the HYDROS mission requirements, baseline design, and measurement capabilities.
Keywords :
antenna feeds; hydrological equipment; ice; microwave measurement; moisture; radiometers; reflector antennas; remote sensing by radar; soil; Earth System Science Pathfinder program; HYDROS mission requirements; HYDROS mission system design; L-band microwave system; NASA; antenna feed system; baseline design; climate prediction; hydrosphere state mission; measurement accuracy; radar electronics; radiometer electronics; reflector; soil moisture; solar illumination; spatial resolution; surface freeze state; surface thaw state; weather prediction; Antenna measurements; Earth; Geoscience; Hazards; NASA; Radar antennas; Soil measurements; Soil moisture; Spatial resolution; Weather forecasting;
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Print_ISBN :
0-7803-8155-6
DOI :
10.1109/AERO.2004.1367701