Type Single seat fighter Single seat fighter "Ente"
Engine 1 HeS 011
Dimensions Length 10,36 m , height  m ,  span  8,25 m, wing area  m2  , Length 9,67 m , height  m ,  span   m, wing area  m2  ,
Weights Empty , loaded  , take off weight    kg
Performance Max.. speed 1015 km/h  , cruising speed  , range , endurance  , service ceiling   , climb Max.. speed 1000 km/h  , cruising speed  , range , endurance  , service ceiling   , climb
Armament 3 MK 108 30 mm provision for two more in the wing roots
  This was the second Messerschmitt design for a high-altitude single-seat fighter. It differed from the Me P.1110/I mainly in the V-tail unit and the annular air intake behind the cockpit. Like the Me P.1110/I, the Me P.1110/II had 40 degree swept-back wings, an HeS 011 jet engine and was armed with three MK 108 30mm cannon in the nose with a provision for two more in the wing roots.
This was another variation of the P.1110 design. The design was of a "duck" (Ente) configuration, that is, small wings (or canards) in front with the larger wing to the rear. This was felt would allow good pitch and lateral stability for low-speed flight characteristics. The air intakes for the single HeS 011 turbojet were located on the fuselage sides, much like the Me P.1110/I. The cockpit was located in the extreme forward fuselage and four MK 108 30mm cannon were located to the sides of the cockpit. Messerchmitt dropped this design in favor of the more conventional P.1110.