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The image provides a "DIAGRAM OF THE DSCS III SATELLITE" showing its various components and their arrangement. Key labeled parts include: a 19 Beam Transmit Multiple Beam Antenna, an Earth Coverage Transmit Antenna, a Satellite to Satellite Interface Fitting (2 of 8), a Solar Array Retention Fitting (2 of 8), an Optical Solar Reflector, a Sun Sensor, a Solar Array Panel Assembly, an Equipment Panel Assembly (North), a Low Noise Amplifier Oven, an Earth Coverage Receive Antenna, a Satellite to Adapter I/F, a Thruster Support, a Gimbal Dish Antenna, an S-Band TT&C Antenna (1 of 2), a Single Channel Transponder Transmit Antenna, an Earth Sensor, a Single Channel Transponder Receive Antenna, and a 61 Beam Transmit Multiply Beam Antenna. The diagram also indicates the satellite's Orbit Direction and a coordinate system with -Y, +X, and +Z axes.
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The diagram illustrates the design and main components of the DSCS III Satellite. Overall, the satellite contains two key parts: solar panels on two sides, and a wide range of antennas in the center.
In terms of two sides of the satellite, it is equipped with solar array panel assemblies, supported by many retention fittings. An optical solar reflector and sun sensor are attached to maximize exposure to sunlight for energy generation. Moreover, the satellite is fixed with a thruster adapter interface to maneuvering. The equipment panel assembly and structure fittings provide further support to these systems.
Regarding the center part, it contains various transit and receive antennas. These include 19 and 61 beam transit multiple beam antennas, earth coverage transit and receive antenna, as well as single channel transponder antennas for both transmission and reception. While a gimbal dish antenna provides an adjustable communication, a low noise amplifier oven ensures signal clarity. In addition, a S-band TT&C antenna is connected with ground stations to exchange data.
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