Name of Infrastructure:

Dornier DO 228-101
 

Description:

The Dornier 228-101 / D-Code serves as an universal flying research platform for various experiments.

Features:

Wing span

16,97 m

Height  

4,86 m

Wing area  

32,0 m²

Empty mass

ca. 3700 kg (without experimental equipment)

Max. TOM

5980 kg

Engines  

2 Garret TPE 331-5

Engine power 

715 SHP Take off power each

Propeller

Hartzell HC-B4TN-5 ML-LT 10574 AB (EL)

VMO

200 KIAS (<15.000 ft) ... 165 KIAS (25.000 ft)

Max. Altitude  

25000 ft (7600 m)

Tank capacity

4156 lbs usable fuel

Average fuel consumption

2 x ca. 300 lbs/h at "normal" operation conditions

 

Application examples:

  • Laminar flow investigation

  • testing of sensors which are capable of creating synthetic outside view,

  • validation of flight guidance systems for traffic flow control on ground and in the air,

  • remote sensing,

  • data link tests. 

     

Target group:

  • Supllier

  • Provider

     

Owner of Infrastructure:

German Aerospace Center
Lilienthalplatz 7
38108 Braunschweig

Tel.: +49 531 295-0

http://www.dlr.de/desktopdefault.aspx/tabid-342/