| Type | Single seat fighter |
| Engine | 2 Heinkel He S 011 |
| Dimensions | Length 12,2 m , height 2,69 m , span 10,6 m , wing area 20 m2 , |
| Weights | Empty , loaded , max. take off weight 7000 kg |
| Performance | Max.. speed 920 km/h, cruising speed , range , endurance , service ceiling 12000 m , climb |
| Armament | 1 MG 151/15 15mm machine gun and 2 MG 213/20 20mm cannons |
This fighter dates from 1943, and was to be of an all-metal construction. It featured swept-back wings, and two He S 011 turbojets were mounted beneath the wings. The fuselage contained three fuel tanks which were located behind the cockpit. A single fin and rudder was fitted with the tailplanes having a small amount of sweep also. The main landing gear rotated 90 degrees before being retracted forwards into the wing. As per the Ar TEW 16/43-13, a spherical tire was chosen for the front landing gear. The cockpit was located in the forward part of the fuselage, and armament consisted of a single MG 151/15 15mm machine gun and two MG 213/20 20mm cannon, all located in the nose beneath the cockpit. This aircraft did not get out of the preliminary design phase; instead, design and production was concentrated on the Ar 234.
