| Technical data | |||
|---|---|---|---|
| Type | UT-2, Ya-2, '20' | ||
| Function | Primary Trainer Prototypes | ||
| Year | 1937 | ||
| Crew | 2 | ||
| Engine | M-11E | M-11E |
Renault Bengali 4 |
| Power (hp) | 150 | 150 | 140 |
| Length (m) | 7.11 | 7.0 | 7.64 |
| Height (m) | ? | ? | ? |
| Wingspan (m) | 10.2 | ||
| Wing area (m2) | 17.2 | ||
| Empty weight (kg) | 574 | 574 | 569 |
| Loaded weight (kg) | 804 | 900 | 888 |
| Wing load | 46.7 | 52.3 | 51.6 |
| Power load | 5.4 | 6.0 | 6.3 |
| Speed (km/h) | |||
| at 0m | 230 | 210 | 240 |
| Landing | 80 | 75 | 85 |
| Roll (m [sec]) | |||
| Landing | 200 [16] |
200 [16] |
263 [20] |
| Takeoff | 150 [12] |
157 [12.5] |
230 [13] |
| Maneuverability | |||
| Turn time | 14sec | ||
| Range (km) | |||
| Normal | 450 | 1000 | 834 |
| Flight Endurance | 2h | 7h | 4h |
| Ceiling (m) | |||
| Maximum | 6500 | 6500 | 6100 |
| Climb (min) | |||
| 1000m | 3.5 | 3.3 | 4 |
| 3000m | 14 | 13.2 | 15.3 |
| Payload | |||
| Fuel+oil (kg) | 60 | 143+ 14.5 |
128+ 15 |
Two-seat monoplane trainer, developed from AIR-10. Unlike the predecessor, UT-2 was all-wooden plane, with Ak g-limit 10. Two prototypes were built, one with 150hp M-11E engine, another - 140hp Renault "Bengali" 4. Both had fuel for 2 hours of flight, what was criticized during State Acceptance Trials. Moreover, aircraft seats did not allow to use parachutes. After the seat modifications and increasing of fuel tank capacity Ya-20 could stay airborne for 7 hours, but it gained 112kg of flight weight and performance was slightly degraded.
Many sources include Ya-20 into the AIR line as AIR-20. But this is a mistake, because no one in its mind could keep naming his product in honor of politician purged by Stalin.
UT-2 with M-11E was rated as 'very good' and recomended for mass production as a primary trainer. Variant with 'Renault' participated in 1937 competitions and took the 1st place, but turned to be a 'dead end' because the engine was not accepted for series production.
Same year UT-2 with M-11E was installed on floats (identical to those of AIR-6). In this configuration it grabbed three International Records.
Mass production of UT-2 started in November 1937 on two factories. Series UT-2 are discussed on other page.
|
|
Drawing by Igor Soultanov, used as a background for this page; ("History of aircraft construction in the USSR") |
| Prototypes | Developments | ||
|---|---|---|---|
|
AIR-10 Ya-10 |
![]() VT-2 - floatplane version |
![]() '20' Ya-20 UT-2 |
|
| References | Links |
|---|---|
|
|
| Created January 25, 1996 Modified January 4, 2002 with help of |
|
Back to Main Gate |