FIELD: transport.
SUBSTANCE: invention relates to pressure garment assembly with temperature control system made up of two circuits: vent circuit and astronaut water cooling circuit. Said vent circuit incorporates CO2 concentration pickups arranged at carbon dioxide absorber cartridge inlet and outlet. Readings of said pickups and those of gas flow rate are used by microcontroller to compute astronaut current power inputs. Special program is used to define required temperature in water cooling jacket to feed appropriate signals to electromagnetic valves arranged in cooled and bypass lines. Opening/closing said valve allows adjusting water temperature in aforesaid jacket.
EFFECT: automatic temperature control system to adjust water temperature in water cooling jacket without interference of astronaut.
4 cl
| Title | Year | Author | Number |
|---|---|---|---|
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