Publication Date:
2016-06-07
Description:
The results of the analysis and the evaluation of flight data obtained from the horizon sensor test project are described. The rotary mechanism of the scanning earth sensor composed of direct drive motor and bearings using solid lubricant is operated satisfactorily. The transmitted flight data from Engineering Test Satellite IV was evaluated in comparison with the design value.
Keywords:
LAUNCH VEHICLES AND SPACE VEHICLES
Type:
JPL The 17th Aerospace Mech. Symp.; p 143-156
Format:
application/pdf
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