Type Single seat heavy fighter
Engine 2 He S 011
Dimensions Length 12 m , height m ,  span  12 m, wing area  m2  ,
Weights Empty , loaded  , take off weight    kg
Performance Max.. speed  , cruising speed  , range , endurance  , service ceiling   , climb
Armament 2 MK 108 30mm
This project became known through a sketch which was published in France after the war. A later well-known drawing suggests that there were two configurations of the same design, although the engine installation and tail design were different. Apparently, it was planned to utilize two He S 011 turbojets which were fed by an air intake located on each side of the fuselage under the wings. To extend range, plans were made to mount two 300 liter auxiliary wingtip fuel tanks. Armament was to be two Mk 108 30mm cannon.