ACU
An
Airborne computer with a 4" LCD screen MFD (Multi Functional Display).
The computer enables to communicate true 8 1553/ ARINC/ RS422 channels with
various of sensors installed on the aircraft. The
computer acts as a mission computer and as a display processor.
The ACU
is designed as one Dzuz-mount LRU, and also as two separate units that can
be installed separately in the cockpit and in an avionics bay. Fully
MIL-STD-810 and MIL-STD-461 designed and tested, the ACU can be ins 22522r174w talled
on any military and civil aircraft. The
ACU is designed for high reliability and maintainability and can be easily
adjusted to customer requirements.
OIT- Oceana Integrated Technologies Ltd. develops and manufactures a broad range of mission critical systems based on various rugged. This quality uniquely positions the company to support the military's near-term force modernization and emerging transformation initiatives. Our unique solution platform which represents the state of the art quality workmanship of our engineers and programmers, can meet specific requirements of individual military customers, delivered in a cost effective and timely manner. OIT high-technology products and services are implemented by various military forces around the globe, all branches of the IDF military, defense prime contractors, international military forces, Homeland security sector and heavy industrial markets.
SPECEFICATIONS
CPU |
Pentium M 1.6 GHz |
|
RAM |
256 MB expandable |
|
DISK |
Flash Disk 2 GB |
|
Operating Voltage |
8 - 32 VDC / 50 W |
|
Serial ports |
2 x USB, 8 x 1553/ ARINC/ RS422/ RS485, Audio, LVDS |
|
Display Unit |
Dzuz mount unit per MS25212 |
|
Screen |
LCD 4" |
|
Brightness |
200 Nit |
|
Resolution |
VGA |
|
controls |
MFD Toggle switches |
|
Physical Characteristics |
(for one LRU) |
|
Weight |
|
|
Dimentions (mm) |
125 (W) x 137.5 (H) x 175 (D) |
|
Interface Connectors |
3 D38999 Connectors |
|
Environmental Conditions |
MIL-STD-810E compatible |
|
Operational Temp. |
-30 - +71 ºC for cockpit LRU -55 - +85 ºC for avionic bay unit |
|
Vibration (random) |
1-2000 Hz, 0.04 g²/Hz, 6.6 gRMS |
|
Shock |
|
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Altitude |
|
|
Other Environmental Conditions |
Rain, Humidity, Fungus, Salt, sand & Dust, Explosive Atmosphere |
|
EMI/EMC |
MIL-STD-461D compatible |
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