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) |
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.
Remark
It is planned to operate as part of a perspective piloted transport system.
Legal information
Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation.
Information on this site may be changed or supplemented.