TYPE: Heavy fighter, fighter bomber. Project
ACCOMMODATION: Pilot only
POWER PLANT: Two Junkers Jumo 004 turbojet engines, rated at 900 kp each or one Heinkel-Hirth HeS 011 turbojet engine, rated at 1,300 kp
PERFORMANCE: No data available
COMMENT: This project became known through a sketch which was published in France after WW II. Probably it dates back to 1942 and suggests a possibility of the”… installation of a radial turbojet engine”. A later well-known drawing suggests that there were two configurations of the same design, the “Zerstörer-Projekt I and II”. In both the air intakes as well as the tail assembly was different. Apparently, it was planned to utilize two Junkers Jumo 004 turbojets or one Heinkel HeS 011 engine. In “Zerstörer-Projekt II” the air intake for the turbojet engines were positioned in the wing roots and the tail plane was swept sharp forward and in “Zerstörer-Projekt II” it was swept back so as the wings. Also the turbojet engine was 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. Two Mk 108 30mm cannon were installed in the nose part. The design was not pursued (Ref.: 16, 17).