Grigorovich TB-5
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Grigorovich TB-5 was an experimental heavy bomber designed and tested in the Soviet Union in the early 1930s. Designed as a competitor for TB-3 TB-5 was intended to be powered by two FAD 24-cylinder X engines of 746 kW (1 000 hp) each. When these were canceled the underwing pods were revised to each house a pair of Bristol Jupiter engines in a push-pull configuration.

(“Rishar”) TOM-1, Grigorovich TB-5, Tupolev Tu-2, Lavochkin La-7R.1
Grigorovich TB-5 (Russian: Григорович ТБ-5) was an experimental heavy bomber designed and tested in the Soviet Union in the early 1930s.2

Grigorovich TB-5 was an experimental heavy bomber designed and tested in the Soviet Union in the early 1930s.3
Jet Or Prop
prop
Designer
Grigorovich (design bureau)
Length Alt
2209.7999999999997
Power Alt
450 hp
Loaded Weight Main
12535.0
Max Speed Alt
6720.0
Type Of Prop
Radial engine
Max Speed Main
180.0
Power/mass Main
107
Bombs
Up to 2
500 kg of bombs
Loading Main
84
Ceiling Main
2
600 m
Number Built
One
Span Main
31 m
Area Main
150 m²
Primary user
Soviet Union
Span Alt
3098.8
Plane Or Copter?
plane
Engine(prop)
Bristol Jupiter V
Status
Retired
Origin
Soviet Union
National Origin
Soviet Union
Loaded Weight Alt
27635.0
Power Main
336.0
Number Of Props
4
Power/mass Alt
252.0
Guns
60.0
Empty Weight Alt
16497.0
Length Main
22.1 m
Area Alt
1614.6
Similar Aircraft
*TB-3*Farman F.220
Empty Weight Main
7483.0
Ceiling Alt
8530.0
Category
Grigorovich aircraft
Soviet bomber aircraft 1930-1939
Loading Alt
17

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