| Technical data |
| Type |
R-5T |
| Function |
Torpedo-Bomber |
| Year |
1933
|
| Crew |
2 |
| Engine |
500/715hp M-17F
|
| Length |
10.60m |
| Wingspan |
15.5m |
| Wing area |
50.2m2 |
| Empty weight |
n/a |
| Loaded weight |
n/a |
| Wing Load (kg/m2) |
n/a |
| Power load (kg/hp) |
n/a |
| Speed |
n/a |
| Range |
n/a |
| Flight Endurance |
n/a |
| Ceiling |
n/a |
| Climb |
| 1000m |
n/a |
| Payload |
| Fuel |
n/a |
| Armament |
| Guns |
2*mg7.62mm PV-1
|
| Torpedo |
1*800kg |
| Bombs |
up to 800kg |
15k b/w section of R-5T landing gear,
"History of aircraft construction in the USSR", Vol.1 p.451
Torpedo-bomber variant with enlarged rudder and radically resided landing gear. New system of (enforced) struts provided all under-fuselage space for torpedo or large bomb. Parking angle increased to 17°. Modification was successful, flight-tested in 1933.
Fifty R-5T were built at Aircraft Factory N°1 and accepted by military in 1935. In service with The Far East Naval aviation until 1938.
| Predecessors |
Modifications |
R-5
|
None |
