| Type | History |
| B-0 | Proposed high-altitude fighter |
| B-1 | Proposed high-altitude fighter |
| Type | Werk.Nr | Registration | History |
| A-3/U7 , B-0 | 528 | Cockpit pressurised. Tested at Rechlin | |
| A-3/U7 , B-0 | 531 | Cockpit pressurised. Tested at Rechlin | |
| A-3/U7 , B-0 | 532 | Cockpit pressurised. Tested at Rechlin | |
| B-0 | 0049 | Cockpit pressurised. GM 1 (85 l tank). Ready for tests in January 1944 Delivered to BMW in April 1944 | |
| B-1 | 811 | Cockpit pressurised. GM 1 (85 l tank, replaced by a 115 l tank to increase the range). | |
| B-1, V 45 | 7347 | BMW 801 D with GM 1 | |
| B-1, V 47 | 530115 | BMW 801 D with GM 1 |
| Type | B-0 , A-3/U7 Single seat high altitude fighter |
| Engine | 1 BMW 801 D2 |
| Dimensions | Length 8,95 m , height 3,95 m , span 12,3 m , wing area 20,30 m2 , aspect ratio 7,45 |
| Weights | Empty 2728 kg, loaded 3850 kg , max. take off weight fuel 396 kg, oil 50 kg |
| Performance | Max.. speed 690 km/h at 6900 m , cruising speed 600 km/h at 7000 m , range 600 km, endurance 1,20 h , service ceiling 11500 m , climb 16 m/srec., landing speed 158 km/h |
| Armament |
