ARC Regulation and Control Equipment for Manned and Cargo Spacecraft

Purpose:
Designed for manned spacecraft.
Year of release: 2012
Guaranteed service life (years): 5
Estimated production / delivery time (months): 18
Flight qualification of the product: No
Possibility to adapt the product to customer requirements: Yes


Parameter Value
Resistance to ionizing radiation of outer space 20 krad
Output voltage (DC) 32 V
Power 2,8 kW
Mass 26 kg
Power density 107 W/kg
Cooling method in vacuum thermal board
Type of interface for commands and telemetry digital
Battery type lithium ion
Setup unpressurized (work in vacuum)

Description

Monoblock equipment for regulation and monitorung of the manned spacecraft’s power supply system. Basic setup includes: - current regulator 4pcs.; - charge-discharge device 4pcs.; - voltage regulator 1pcs.; - central control submodule 1pcs.; It is possi
... Monoblock equipment for regulation and monitorung of the manned spacecraft’s power supply system.
Basic setup includes:
- current regulator 4pcs.;
- charge-discharge device 4pcs.;
- voltage regulator 1pcs.;
- central control submodule 1pcs.;
It is possible to change the design of the monoblock to increase power up to 10 kW by layout of internal submodules.

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Remark

It is planned to operate as part of a perspective piloted transport system.

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