Blohm & Voss BV P.170

BV P.170  3 view    This fighter-bomber was designed by Dr. Vogt of Blohm und Voss in 1942, designer of the BV 141 and other asymmetric designs. Although the BV P.170 was of a symmetrical design, it was still unorthodox in appearance. The wing was of constant chord, and contained the ailerons and landing flaps, which were to be constructed of wood or a light metal. Three BMW 801D radial engines (rated at 1600 horsepower each) provided the power; each drove a three-bladed 3.5 m (11' 5") propeller. One engine was located on the front of the main fuselage, while the other two were mounted on wingtip gondolas, each with a single vertical fin and rudder located at the rear. Each engine gondola (including the center fuselage) contained a 2000 liter (528 gallon) fuel tank, which could only feed the engine ahead of it. The two outside engines rotated in opposite directions, to help cancel out excessive torque. The two man crew (pilot and radio operator/ observer/ bombadier) sat in a cockpit located in the extreme rear of the center fuselage, of which there were two main designs. A normal "tail-dragger" undercarriage was fitted, with the exception of there being three main landing gear legs (1015 x 380 mm wheels were to be fitted to each leg), one located just aft of each engine. Each main landing gear leg retracted to the rear into the engine nacelle or main fuselage. 2000 kg (4400 lbs.) of bombs could be carried in underwing mountings. The project's speed was thought to preclude interception, thus no defensive armament was to be fitted.

      Kevin Wafer's BV P.170 art images

Blohm & Voss BV P.170.01 Dimensions
 Span Length Height Wing Area
16.0 m 
52' 6"
14.3 m 
46' 11"
3.65 m 
12' 0"
44.0 m² 
473.6 ft²
 
Blohm & Voss BV P.170.01 - Weights
Empty Weight (Equipped)  Crew Fuel Equipment Bombs Flying Weight Wing Loading
9100 kg 
20062 lbs
200 kg 
441 lbs
2800 kg 
6173 lbs
450 kg 
992 lbs
1000 kg 
2205 lbs
13300 kg 
29321 lbs
302 kg/m² 
61.9 lbs/ft²
 
 Blohm & Voss BV P.170.01 Performances
Max. Speed Rate of Climb Takeoff 
Speed
Landing 
Speed
Max. Ceiling Range
@ 0 km 
0 ft
610 km/h 
379 mph
@ 2 km 
6562'
675 km/h 
419 mph
@ 4 km 
13123'
695 km/h 
432 mph
@ 6 km 
19685'
760 km/h 
472 mph
@ 8 km 
26247'
820 km/h 
510 mph
@ 10 km 
32808'
715 km/h 
444 mph
 
@ 0 km 
0 ft
17.8 m/s 
58.4 ft/s
@ 2 km 
6562'
18.9 m/s 
62.1 ft/s
@ 4 km 
13123'
14.6 m/s 
47.9 ft/s
@ 6 km 
19685'
14.9 m/s 
48.9 ft/s
@ 8 km 
26247'
11.3 m/s 
37.1 ft/s
@ 10 km 
32808'
5.2 m/s 
17 ft/s
 
181 km/h 
113 mph
156 km/h 
97 mph
11650 m 
38222'
2000 km 
1243 miles
 
Blohm & Voss BV P.170 Models
Manufacturer Scale Material Notes
CzechMaster (CMK)    #274 1/72 resin Kit models April 4, 1942 cockpit design version 
Two SC 1000 bombs included

Two drawings of the BV P.170 in action from the 
original Blohm & Voss proposal to the RLM - 1942
 
Two different cockpit designs for the BV P.170 
 
Top: design dated April 4, 1942 
Bottom: design dated September 17, 1942
Bombloads for the BV P.170
Normal Load
Number Type Total Weight Location
1 SC 1000 1000 kg under starboard wing
2 SC 500 1000 kg one under each wing
4 SC 250 1000 kg two under each wing
Over Load
Number Type Total Weight Location
2 SC 1000 2000 kg one under each wing
4 SC 500 2000 kg two under each wing
 
 
Original Blohm & Voss proposal
Large format 3-view drawing of the BV P.170
 

BV P.170 color side view
 

  The BV P.170 in winter colors as it might have appeared as a fighter-bomber on the Eastern Front....
 
 
 

                From ReichDreams Dossier #13, Asymmetric Planes by J. Miranda & P.Mercado