MIRAH-development and -approval
Christian Linke during the preparation of individual components
Hans-Peter Heuser in the construction of a wiring harness
Marc Krebsbach during the assembly of a container module
View of the compressor box
The diaphragm pump insert from the rear
Electronic unit with fixed laptop
MIRAH after final assembly in the laboratory
The container module rack with 24 sampling cylinders
Back view of the container module rack
MIRAH in the EMV test (1)
MIRAH in the EMV test (2)
MIRAH in the EMV test (3)
MIRAH in the EMV test (4)
MIRAH in the EMV test (5)
MIRAH in the EMV test (6)
MIRAH in the EMV test (7)
MIRAH in the EMV test (8)
MIRAH in the EMV test (9)
MIRAH in the EMV test (10)
MIRAH in the EMV test (11)
MIRAH in the EMV test (12)
MIRAH in the EMV test (13)
MIRAH in the EMV test (14)
Cabin of the HALO (view towards the cockpit)
HALO cabin (view towards the rear / luggage compartment)
Cable routing during test installation
Test installation of MIRAH in the HALO luggage compartment (1)
Test installation of MIRAH in the HALO luggage compartment (2)
Test installation of MIRAH in the HALO luggage compartment (3)
Test installation of MIRAH in the HALO luggage compartment (4)
Test installation of MIRAH in the HALO luggage compartment (5)
Test installation of MIRAH in the HALO luggage compartment (6)
Test installation of MIRAH in the HALO luggage compartment (7)
Test installation of MIRAH in the HALO luggage compartment (8)
Test installation of MIRAH in the HALO luggage compartment (9)
Burst test of a sampling tank (before)
Burst test of a sampling tank (after)
The container was broken at 240 bar
