Overview
This unit has been design for cockpit installation (DZUS Mounting), with a quick access to the memory cartridge for post flight analysis. This system is capable to record High definition video/audio (720p/i or 1080p/i) or lower resolution PAL/NTSC, digital data bus(MIL-STD-1553, ARINC 429 ...) and analog data (Like strain gauges, Discrete...) .
- Lightweight mission recorder
- Quick access recorder (QAR)
- From 8GB to 256 GB
- Full NVG/night/day compatibility
- Qualified MIL-Spec for airborne use
- Panel mounted with DZUS fasteners
- Events marker
Technical specifications
Size (D x W x H)
190mm x 146mm x 85.7mm
Weight
About 1.4 Kg
Input Connector
MICRO D (MIL-DTL-38999)
Mounting
DZUS
Power supply
28Volts DC (16 to 36V) MIL STD704 E Consumption: 12 watts nominal. Ultra capacitor "to preserve recorder of power cuts (power interruption >100ms)
Grounding
Electronics electrically isolated of the primary 28 Volts supply. GND electronics is also isolated of the DTMUX-M2 external box.
Cooling
Passive convection
Position of use
All positions
MTBF> 30 000 hours
MTTR< 30 minutes
Transport
Delivered with a transport suitcase equipped to receive the DTMUX-M2 and accessories.
190mm x 146mm x 85.7mm
Weight
About 1.4 Kg
Input Connector
MICRO D (MIL-DTL-38999)
Mounting
DZUS
Power supply
28Volts DC (16 to 36V) MIL STD704 E Consumption: 12 watts nominal. Ultra capacitor "to preserve recorder of power cuts (power interruption >100ms)
Grounding
Electronics electrically isolated of the primary 28 Volts supply. GND electronics is also isolated of the DTMUX-M2 external box.
Cooling
Passive convection
Position of use
All positions
MTBF> 30 000 hours
MTTR< 30 minutes
Transport
Delivered with a transport suitcase equipped to receive the DTMUX-M2 and accessories.
Environmental specifications
Vibration
MIL STD810F 0.04 g² of 5 to 1000 Hz, 1 hour per axis (3 axis
Accelerations
MIL STD 810F 1/2 sinus, > 60 g, 11ms (6/2 axis) in functioning
Shocks
MIL STD 810F/ RTCA/DO-160E 1/2 sinus, > 60 g, 11ms (6/2 axis) in functioning
Operating Temperature
- 40°C to + 71°C.
Extreme operating temperature
- 55°C to + 85°C [no destructive] Test MIL STD 810F
Humidity in use
5% to 95 % without condensation MIL STD 810F
Electromagnetic compatibility (EMI)
MIL STD 461 Rev. F (10/12/2007) MIL-STD-464 Rev. C (01/12/2010)
Altitude and decompression
Min: -1500 feet, max: 60,000 feet
With 12.000 feet/minute
(420 Kpa/minute), MIL STD 810F.
Altitude max. storage
No limit
Storage temperature
- 55°C to + 90°C
Humidity in storage
5% to 95 % without condensation MIL STD 810F
Aircraft Electrical Power Characteristics
MIL-STD-704F
Power down 100 millisecond
MIL STD810F 0.04 g² of 5 to 1000 Hz, 1 hour per axis (3 axis
Accelerations
MIL STD 810F 1/2 sinus, > 60 g, 11ms (6/2 axis) in functioning
Shocks
MIL STD 810F/ RTCA/DO-160E 1/2 sinus, > 60 g, 11ms (6/2 axis) in functioning
Operating Temperature
- 40°C to + 71°C.
Extreme operating temperature
- 55°C to + 85°C [no destructive] Test MIL STD 810F
Humidity in use
5% to 95 % without condensation MIL STD 810F
Electromagnetic compatibility (EMI)
MIL STD 461 Rev. F (10/12/2007) MIL-STD-464 Rev. C (01/12/2010)
Altitude and decompression
Min: -1500 feet, max: 60,000 feet
With 12.000 feet/minute
(420 Kpa/minute), MIL STD 810F.
Altitude max. storage
No limit
Storage temperature
- 55°C to + 90°C
Humidity in storage
5% to 95 % without condensation MIL STD 810F
Aircraft Electrical Power Characteristics
MIL-STD-704F
Power down 100 millisecond
Modules and options
-
Digital/Bus Modules
- PCM Acquisition/Restitution v
- serial FPDP (Fiber) 3
- ARINC 429 v
- MIL-STD-1553 v
- AFDX® / ARINC 664 3
- Stanag 3910 v
- Ethernet 3
- CAN bus v
- Differential discrete v
- Pulses Measure/Counter v
- PCM Merger v
- RS 422/485 v
- RS 232 v Video/Audio Modules
- Video SD $
- Video HD $ Accessory(ies)
- HD Camera & Area Mic combo
- Crash protected memory unit
