Figure 4.8. Theoretical (1) and experimental (2) dependences of parameters during testing of the Soyuz APDA (impact with displacement), a. longitudinal force acting on body 1; b. transverse force acting on body 2; c. transverse displacement of ring; d. longitudinal displacement of ring; e. rotation of ring relative to axis z. A [contents of box] t = 12.06-contact; t = 13.63-linkage; V* — 0.3 m/s; = 0.07 m/s; At/ = 0.3 m; A8 — 5'; 0* = 0.07 deg/s; B. kgs; C. m; D. degrees; E. seconds.
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