T/G Layout 1

(C. Jardin) #1

Solar Panel


Primary source of spacecraft electrical power, designed so
that normal satellite day light operation, plus required
battery charging power can last for approximately seven
years


Sun Sensors


Provides information on spacecraft spin rate and attitude
with respect to the sun line, and provides reference pulses for
the VAS system


Thermal Barrier


Assists in thermal control, which is accomplished by using passive energy
balance techniques


Ultra High Frequency (UHF) Antenna


Used to receive Earth-based data


VISSR Atmospheric Sounder (VAS)


See next page


VAS Sunshade


Shades the VISSR Atmospheric Sounder


X-Ray Sensor (XRS)


Uses ion chamber detectors to measure ionospheric effects associated with solar flares

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