Type Two seat fighter
Engine 2 He S 011
Dimensions Length 12 m , height 3,38 m ,  span  12,58  m, wing area 15,3 m2  ,
Weights Empty , loaded  , take off weight   kg
Performance Max.. speed 778 km/h , cruising speed  , range , endurance  , service ceiling   , climb
Armament
This more advanced version for the Me P.1100 was proposed in March 1944. It was to have the 45 degree swept back wing that was developed for the Me 262 HG III project. Two He S 011 A turbojets were buried in the wing roots, and the cockpit held a crew of two. A final project, dated May 7, 1944 was for a version with increased wing span. There were several armament variants proposed (see table below). Although Siegfried Knemeyer (chief of development for the RLM Technical Department) expressed considerable interest in the project and inspected several mockups, they were eventually cancelled in 1945 due to the thought that the P.1099 and P.1100 projects were underpowered.