Blohm & Voss BV P210 ``Volksjager``
This was one of Blohm & Voss' entries in the Volksjäger Project competition in September 1944. Chief Designer Dr. Richard Vogt, assisted by Hans Amtmann, developed the BV P.210 from the BV P.208 tailless fighter project. The P.210 featured Blohm & Voss' usual tubular spar, which was the central air duct from which the other components were attached. The wings were swept back at 30 degrees, and had dihedral on the main wings with drooping wing tips. A single BMW 003A-1 jet engine provided the power, there was also optional rocket takeoff assistance. The landing gear was of a tricycle arrangement, with the main gear being attached to the wing spars and retracting inwards and the front gear rotated 90 degrees to lie flat beneath the air intake duct. Armament was to be either two MG 151/20 20mm cannon or two MK 108 30mm cannon in the nose
more pictures here https://www.google.rs/search?q=blohm+%26+voss+p210&espv=2&biw=1366&bih=659&source=lnms&tbm=isch&sa=X&ved=0ahUKEwi5rqKhpI3KAhVK7BQKHdm4BvIQ_AUIBigB&dpr=1
Specifications
General Characteristics
- Created On Windows
- Wingspan 47.3ft (14.4m)
- Length 24.2ft (7.4m)
- Height 6.6ft (2.0m)
- Empty Weight 4,243lbs (1,925kg)
- Loaded Weight 5,569lbs (2,526kg)
Performance
- Power/Weight Ratio 2.017
- Wing Loading 33.2lbs/ft2 (162.3kg/m2)
- Wing Area 167.5ft2 (15.6m2)
- Drag Points 2368
Parts
- Number of Parts 31
- Control Surfaces 8
- Performance Cost 204