| Technical data | |
|---|---|
| Type | M-102 'Duet-Saras' |
| Function | Passenger, Business |
| Year | ? |
| Crew | ? |
| Engines |
2*1500hp TVD-20M 'Mars' or Pratt&Whitney PT6A-67 |
| Length | ?m |
| Wingspan | ?m |
| Wing area | ?m2 |
| Empty weight | ?kg |
| ?Loaded weight | ?kg |
| Wing Load (kg/m2) | ? |
| Power load (kg/hp) | ? |
| Speed at 0m | ?km/h |
| Speed at m | ?km/h |
| Landing Speed | ?km/h |
| Landing Roll | ?m ?sec |
| Takeoff Roll | ?m ?sec |
| Range | ?km |
| Flight Endurance | ?h?min |
| Ceiling | ?m |
| Climb | |
| 1000m | ?min |
| Payload | |
| Fuel | ?kg |
| Seats | 14 |
| Cargo | ?kg |
M-102 'Duet-Saras', A.Bruk Myasichev KB
 |
Twin-pusher turboprop passenger aircraft, joint project with the National Aerospace Laboratory of India. It is designed for short-range hot (up to 45° and high (up to 2000m) operations, and may be powered by Pratt&Whitney PT6A-67 engines for export or Mars TVD-20M for use in the CIS.
Expected market is ~300 of the aircraft in India, at a unit cost of US$3.5-4 million.
Project passed through severe financial problems in 1995-1997.
The Smolensk Aviation Plant JSC has produced an airplane mockup, presented here.
| Predecessors | Modifications |
|---|---|
| References | Links |
|---|---|
| ... |
|
