Spacecraft Disturbance Test

Physics

Scientific paper

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Hst Proposal Id #4435

Scientific paper

This test will verify the absence or presence of thermally induced spacecraft disturbances with the Solar Array 2 wings installed. It will provide information on the locations and nature of the disturbance. The test requires that data be taken with the spacecraft in two attitudes: 1) +V3 to the Sun 2) -V1 to the Sun (as close as possible given operating constraints) In both cases, the solar array panels shall be normal to the Sun.

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