Abstract
A flight model of the free-space laser communications terminal onboard the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) was well developed by the National Space Development Agency of Japan, and the Proto-Flight Test was over in January 2001. At present, the flight model of the satellite is stored in the manufacturer and waiting for its launch. The system level test of the satellite is conducted every 6 months, and the movable devices are turned on every 3 months during this storage period. The optical pointing and tracking characteristics of a laser communications terminal called the Laser Utilizing Communications Equipment (LUCE) are tested again as the terminal level test in the thermal vacuum test. The pointing and tracking accuracy, the far-field pattern of the laser transmitter, the bit error rate, and so on are verified in this reconfirmation test. The acquisition time is also measured in the ambient and vacuum conditions. The LUCE terminal maintains the optical performances in order to establish the optical inter-satellite communication link between the OICETS and an European experimental data relay satellite.
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