Figure 1.9. Schematic of docking control. 1. system of active spacecraft; 2. docking control block; 3. active docking assembly; 4. passive docking assembly; 5. passive spacecraft system, a. system of electrical power supply (27 V); b. telemetry; c. cosmonaut's panel; d. control of systems; e. radio command line; f. entry, exit; g. switch off; h. control system; i. 27 V; j. telemetry; k. commands; I. signaling; m. supply; n. commutation; o. logical processing of temporal monitoring; p. firing of docking mechanism; q. communications; y. contact sensor 1; z. contact sensor 2; aa. DS [expansion unknown]; bb. docking mechanism drive; cc. terminals; dd. DSS [expansion unknown]; ee. pyrotechnic cartridges; ff. electrical connectors; gg. pyrotechnic bolts; hh. firing of latches of socket; ii. DSP [expansion unknown]; jj. telemetry. “entrance” engines of the jet control system are turned off and the engines for the “exit” of the active spacecraft from the passive are activated. Commands to turn the jet control system on and off are issued by an autonomous time mechanism which is actuated at first contact.
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