Figure 1.5. Schematic of the verification and adjustment of targets (APDA). a. equipment for docking the command module and the docking module; b. equipment for docking the Soyuz and Apollo spacecraft. 1. docking mechanism on the command module; 2. target adjustment; 3. adjustment to command module visor imitator; 4. target; 5. frame of the rocket booster; 6. receiving cone on the docking module; 7. Apollo spacecraft imitator; 8. adjustment to visor imitator; 9. APDA; 10. target on the Soyuz spacecraft. Table 1.1. Initial docking conditions for designing docking devices, a. Docking device projects; b. m/s; c. m; d. degrees; e. degrees/second; f. Soyuz-Salyut; g. Gemini-Agena; h. Apollo-Skylab; i. APDA; j. APDA after changes.
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