| Type |
V1 Single seat fighter |
V2 Single seat fighter |
V3 Single seat fighter |
| Engine |
1 Rolls-Royce Kestrel VI |
1 Rolls-Royce Kestrel V |
1 Junkers Jumo 210C |
| Dimensions |
Length 10,30 m, height 2,65 m, span 10,89 m, wing area 21,0 m2 |
|
Length 10,10 m, height 2,75 m, span 11,80 m, wing area 21,0 m2 |
| Weights |
Empty , loaded , max. take off weight |
Empty weight 1642 kg, flying weight 2125 kg |
Empty weight 1645 kg, flying weight 2100 kg |
| Performance |
Max.. speed , cruising speed , range , endurance , service ceiling , climb |
Max. speed 415 km/h at 2700 m, range 800 km, rate of climb 9,5 m/sec. ???? |
Max. speed 435 km/h ?? |
| Armament |
2 7.92mm MG 17 machine guns (proposed) |
| Type |
Werk.Nr |
Registration |
History |
| V1 |
861 |
D-ILOH ? |
First flight 26 July 1935. Ready for testing in July 1935, crashed soon when testing spin at Brandenburg, the pilot Schröder was saved by the parachute |
| V2 |
862 |
D-IMEM ? |
First flight in octber 1935. Oct. 1935 with a Rolls-Royce Kestrel engine, probably from the V1. Later a Junkers Jumo 210C was used. Got an enclosed cockpit.(as D-IMEM) |
| V3 |
863 |
D-IROK ?
|
First flight in July 1937. Dec. 1935, had a Jumo 210C with a variable pitch propeller. Tested Fowler flaps and different cannon arangement firing through the prop.hub. Rebuilt with a straight wing (as D-IPBN |
| V4 |
|
D-INEI, D-ILNI ??? |
Got a Jumo 210 (as D-ILNI), Probably rebuilt V2 orV3 |
| V5 |
1297 |
D-IPBN ? |
Two seater. Used in 1940 for testing a safety device to restrict all rudders during high speed |
