Vladimir S. Syromiatnikov Spacecraft Docing Devices deom SSI

Figure 2.2. Plan for the matching of locks of the docking frame (APDA). a. load, kg; b. deformation, mm. active clamp; c. kg/mm max.; d. kg/mm min.; e. total deformation of clamp installed on the docking frame versus load; f. deformation, mm, passive clamp; g. course, mm; h. course of active clamp; i. extension of passive clamp above joint plane; j. max.; k. min; 1. extension of active clamp above joint plane; m. course of passive clamp and deformation of structure at force of 2500±30 kg; n. extension of passive clamp above joint plane; o. plane of joint; p. passive clamp; q. conjugation; r. active clamp; s. axis of active clamp; t. only these surfaces should be covered with a solid lubricant 0.015 mm thick. The dimensions are monitored after coating. The presence of a coating on the remaining surfaces of the clamp is permitted. ~!A

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