Largest Airborne Observatory in the World equipped with MPL Switches (MAGBES)

Rugged embedded switch used in extended temperature enviroment.

• Universal 10-port switch
• Built in 19" 1U rack
• All ports on M12 connectors
• Extended temperature operation (-40°°C to +85°C )
• Low power consumption, <6W with use of 10-ports
• Convection cooled, dust protection
• Long-term available (+10 years)

Avionics , Defense, Communication
Fanless open frame Swap-C solution with i7 and NVIDIA GPU

Rugged solution to be installed on helicopters

• i7, Quad core with NVIDIA CPU (MXM)
• All conductive cooled
• Long term available
• Proven solution with multiple expansions
• ECCDDR on CPU board
• All interfaces are available on lockable headers
• GRIP with MXM board
• SATA drive with hardware erase

Avionics & Defense Application
Airborne Mission Networking Avionics Interface

• Rugged embedded i7 CPU
• Extended temperature -40°C to +55°C
• 2 second hold-up time (programmable)
• 48x DIOs, 12x serial lines, 2x GigE, 2x ARINC 429
• 1x 1553 redundant, 1x 1553 transmit inhibited
• 4x EIA 530 synchronous serial Interface
• IP67 housing with 10x D-38999 connectors, all on one side
• SWaP-C (220 x 296 x 120mm)
• Removable SSD

Avionics & Defense Application
Combat System Operator system for AC-130J

• Rugged embedded i7 CPU
• Extended temperature -40°C to +55°C
• 2 second hold-up time (programmable)
• 16x DIOs, 4x serial lines, 2x GigE, CAN Bus
• 2x 1553 redundant, 2x 1553 transmit inhibited
• IP67 housing with 8 x D-38999 connectors
• SWaP-C (265 x 292 x 71mm)
• Removable SSD

Avionics & Defense Application
Mission Management Computer (MMC)

Used on various aircraft

• Rugged embedded i7 CPU
• Extended temperature -40°C to +55°C
• 2 second hold-up time (programmable)
• 48 DIOs, 16 serial lines, 2x GigE, CAN Bus
• 2x 1553 redundant, 2x 1553 transmit inhibited
• IP67 housing with 10x D-38999 connectors
• SWaP-C (265 x 292 x 71mm)
• Removable SSD

Avionics & Defense Application
Embedded Voice over IP Interface Processor

Used on UAV and other aircraft

• Rugged embedded i7 CPU
• Extended temperature -40°C to +55°C
• 100ms hold-up time
• 4x E1 interface on XMC
• Removable SSD
• IP67 housing with 5 x D-38999 connectors
• SWaP-C (238 x 188 x 73.2mm)
• MIL-STD-810 and DO-160 testing

Avionics & Defense Application
Real-Time Data Acquisition Test Set

• Rugged embedded i7 CPU
• Integrated UPS system
• ARINC 429 and 1553 interfaces on XMC
• Digital I/Os galvanic isolated
• Analog 12bit I/Os
• IP67 housing with 8x D-38999 connectors
• SWaP-C (296 x 220 x 103mm)

Onboard Computer for a stratospheric balloon

The CEC14 is responsible for all data collected by the balloon in the stratosphere at an elevation up to 45km.

• Compact Atom Computer / Quad Cores
• ECC RAM
• Linux OS
• Each unit tested in climate camber at -40°C up +85°C
• Supplied as Open Frame solution (for easy integration in existing cabinet)
• Long term availability and serviceability

Internet & Live TV on Business Jets

• RTCA DO-160 & RTCA/DO-178 compliant
• - 55°C operational
• Two band satellite communication
• Vertical connector for GigE interface
• Install of Atlta DT ARINC 429 miniPCIe module
• MAGBES-21HS on top
• Linux OS with Real Time patches

Airborne Control PC with flexible data storage units

• Digital modular system for aerial image acquisition
• Used in helicopters and fixed-wing aircrafts
• PIP11 used in a user specific compact housing, board mounted on cooling plate
• Connected to the PIP:
  - over FW up to 2 digital cameras with 39Mpixel
  - over SATA two storage units for 6400 images
  - over DVI & USB a 8 inch TFT touch-screen

Airborne Sensor control and data logging system

• 3D laser measurements of the earth´s surface
• Used in helicopters and fixed-wing aircrafts
• Standard PIP11 with flange, mounted on shock absorbing platform
• The PIP manages and controls the "Light Detection and Ranging unit" and acts as data logger during airborne missions

Data Transfer Device

• Commercial & Military aircraft use, for distributing mission data over PCCard or SATA drives to all mission systems
• IBM440 GX/666MHz PowerPC, 10.5 Watts, 4x SATA , 3x GigE Ports, ...
• Low power consumption ext. Temperature
• Long-term availability

Wireless Communication Space Shuttle

• Used in Space Shuttle & ISS Operations
• Key points: low power design, rugged design, multiple SW support (Linux, RT Linux, VxWorks) reliability, support and test results (radiation environment)

Storage Controller in Avionics Program

• Data storage and data communication during mission
• Used in various airplanes
• Key points: ruggedness, extended temperature, support, flexibility (semi custom), long-term availability
• VxWorks & Linux OS support

MIR Interface System to payload system

• Interfaces Payload-Systems to the Tele-metry-System in the Space-Station MIR
• MC-DISK-E
• Launched May 94 with a Proton Rocket, returned August 96 with STS-79 Space shuttle

Data Acquisition on airplanes

• Custom development around the IBM405 CPU, onboard Flash & RAM
• The CPU board is used as avionics computer in a PC/104-Plus stack
• Extended temperature design for -40°C up to +85°C
• Due to the broad experience MPL was selected to develop the specific board, which is coated according customer requirement

PIP installed in helicopter

• The heat scan camera is connected to the embedded PC installed on board the helicopter
• The system can detect warm spots on earth, lost humans in the forest, hot spots of fire, as well as victims in avalanches
• Key decision factors: compactness, flexibility of the system, amount of features. The product comes with extended temperature