Description
Part of the industry-leading line of high performance chassis and backplane solutions, this ruggedized liquid-convection cooled ATR solution (Solution 61-174) was designed to meet customer requirements for an airborne ISR application. The enclosure is a 1+ ATR chassis designed to perform in 0-20,000 ft and -10 to +50°C environment. The chassis supports 3-phase MIL-STD-704F 115VAC input with a MIL-STD 704F compliant 900W power supply. The 1+ ATR enclosure is forced liquid-cooled and supports air-cooled OpenVPX payload boards. The backplane supports 8x 6U OpenVPX slots and 2x 3U OpenVPX slots of 1.0″ pitch. This ATR enclosure includes an OpenVPX hybrid 3U/6U backplane, liquid-cooled power supply, and liquid-air heat exchanger.
Features
- Modified ATR form factor: 12.25″ x 14.00″ x 17.5″ (H x W x D), not including handles, connectors and fan assembly (+3.74″)
- Unusual liquid/air heat exchanger solution allows use of air-cooled payload in rugged airborne applications
- Liquid-cooled chassis and power supply
- Supports air-cooled chassis payload with re-circulating cooling air utilizing liquid/ air heat exchanger and internal MIL grade fans
- Application-specific 10-slot hybrid 3U/6U OpenVPX backplane:
- (10) OpenVPX 1.0″ pitch slots
- 8 slots 6U OpenVPX
- 2 slots 3U OpenVPX
- Liquid-cooled using PAO
- -10 to +50°C
- 0 to 20 kft
- 3-phase 115VAC input MIL-STD-704F 900W power supply
- Elapsed time indicator
