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 | The two-impellent uchebno-training plane with coupled steering wheel management. Placing of pilots nearby
The plane of the normal scheme in the plan, the mixed design. The chassis three-rack-mount with a nasal rack. Mechanisation covered - a simple flap.
Product cost: from 39500 USD. | Mass and centering characteristics. | | Take-off weight, kgs | 730 | | Weight of the empty, kgs | 470 | | Oil, kgs | - | | Antifreeze, kgs (Air cooling) | - | | Equipment, kgs | 3 | | Weight of the equipped plane, kgs | 473 | | Fuel, kgs | 50 | | Crew, kgs | 80 | | Useful loading, kgs | 128 | | Centering of the equipped plane, % САХ | 27 | | Extremely forward centering, % САХ | 25 | | Extremely back centering, % САХ | 38 | Letno-technical characteristics. (A power-plant on the basis of RMS-500 with reducer i=2.61,
Electrostarter, resonant pipe, ВВ)
| | Speed of the beginning of jolting , km/hour | 60 | | Speed, km/hour | | | - separation (with flaps 25 degrees ) | 65 | | - ascent | 90 | | - the cruiser | 130 | | - maximum in horizontal flight | 150 | | - landing approach | 95 | | - landing (with flaps 40 degrees ) | 55 | | Speed of lifting the maximum, m/second | | | - in a cruiser configuration / at speed | 2,5m/s 90km/hour | | Length of running start, m. | 170 | | Running start time, second | 12 | | Length of run, m. | 60 | | The maximum range of flight, km. | - | | - at speed, km/hour | - | | The maximum duration of flight, hour | 2.5 | | - at speed, km/hour | - | | Max. an operational overload, +ny | 6 | | (at G max) - ny | 3 |
The two-impellent plane
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