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AMC-800 - Airborne POD Computer
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Extended Temperature
available from -55°C to + 71°C
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Miniature Airborne
PC computers running Embedded Windows XP.
AMC-800 computers are built
and qualified for F-15, F-4, A-4, F-5 and F-16 "Wing Tips".
The AMC-800
options include various input output cards, Flash disk recording.
AMC-800,
PC features AMD Geode™ LX800 @ 500 MHz, 256MB CPU, SoundBlaster,
Ethernet, MIL-1553 or MIL-STD-1760, RS-422/RS-232, Discrete
signals, and GPS
processing. The major hardware components of the AMC-800, are:
256MB RAM
2GB
Disk On Chip, XP Embedded
100BaseT Ethernet
2 x RS232/RS422/RS485
4 x USB 2.0 host
PCMCIA Drive
SoundBlaster with output impedance
8 ohm or 50Kohm
MIL-STD-1553 or MIL-STD-1760 Bus controller,
Remote-terminal,
Bus-monitor
Expansion slots.
Dimensions -
250x100x90[mm] 10"x4"x4"
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250 x 100 x 90 [mm]
2.2Kg |
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Power Supply requirements
5VDC 4A, +12VDC .3A, -12VDC 0.1A or
28VDC according to MIL-STD-704A
AMC-800,
Construction
The AMC-800, is designed and
constructed in accordance with the general requirements of MIL-STD-454.
Thermal
Design
The
cooling of the components on the AMC-800, is accomplished by heat conduction from
its surface.
Moisture
and Fungus Resistance
AMC-800, assemblies are moisture resistant and are not nutrients for fungi. The
components are
treated with
Conformal coating for protection. The coating conforms to MIL-I-46058C.
External
Finishes
The
computer external surfaces are chemically treated prior to painting.
External
Connectors
External
connectors are used for interfacing with the subassemblies or equipment and
are in accordance with
requirement of
MIL-STD-454. Connector mating bodies are keyed, and
keyed
locations are varied to prevent improper installation.
Identification
and Marking
The
marking and labels of the equipment meet the requirements of MIL-M-13231.
Environmental
Conditions
Temperature
The AMC-800, will not be damaged or affected by the effects of ambient air temperature as follows:
Operating:
The AMC-800, shall meet performance requirements specified herein
after exposure to temperatures from
-54°-71°C
(85°C
for intermittent operation).
Non-operating:
(Storage and transportation) -54°-95°C.
Relative
humidity
AMC-800, in an operating or
non-operating condition, shall not be affected by humidity for both continuous
and intermittent periods, including conditions wherein condensation takes
place in and on the equipment in
the form of water.
Operating:
95% relative humidity (RH) with no condensation.
Non/operating:
95% RH.
The AMC-800, meets the requirements specified in MIL-STD-810E.
Vibration
The AMC-800, has been tested according to MIL-STD-810E for airborne environment.
Shock
The AMC-800, operates as specified herein after being subjected to operational
shock according to MIL-STD-810E, 40 g for duration of 11msec.
Fungus
The AMC-800, is non-nutrient to fungus growth. It
meets the requirements specified in MIL-STD-810E.
Sand
and Dust
The AMC-800, shall operate as specified herein while and after being
subjected to sand and dust as encountered in dry arid
areas. The AMC-800, shall meet the
requirements specified in
MIL-STD-810E.
Salt
Fog
The AMC-800, is resistant to the corrosive effects of salt fog environment. The
AMC-800, meets the requirements specified in
MIL-STD-810E Method 509.3 Procedure
I. The base metal shall not be visible through the finish or
coating, nor shall there be any
evidence of blistering, softening, separation from the base metal,
corrosion products, or
other coating failure.
Interchangeability
The
components of the AMC-800, are physically and functionally interchangeable in accordance
with MIL-STD-454. Parts
or components of the same part number procured
to
this specification are physically and functionally interchangeable without selection,
adjustment
or fit.
Maintainability
and Modularization
AMC-800, is designed such that it is
completely maintainable by replacement of assemblies.
Maximum
use is made of
plug in module assemblies.
Reliability
AMC-800,-PC has an MTBF of 10,000 hours at 25°C . Mean
Time To Repair (MTTR) does not exceed 30 minutes. The
MTTR includes the time required to detect and isolate the failure, replace the failed
unit, checkout the repair and
return the system to full
operational
status.
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