| Technical data | |
|---|---|
| Type | ANT-2 |
| Function | Passenger Technology demonstrator |
| Year | 1923 |
| Crew | 1 |
| Engines | 1*100hp Bristol-Lucifer |
| Length | 7.50m |
| Wingspan | 10.0m |
| Wing area | 17.5m2 |
| Empty weight | 523kg |
| Loaded weight | 836kg |
| Wing Load (kg/m2) | 47.5 |
| Power load (kg/hp) | 8.36 |
| Speed at 0m | 170km/h |
| Speed at 3000m | 155km/h |
| Landing Speed | 78km/h |
| Landing Roll | 6sec |
| Takeoff Roll | 8sec |
| Range | 425km |
| Flight Endurance | 2.5hmin |
| Ceiling | 3300m |
| Climb | |
| 1000m | 8.5min |
| 2000m | 21.5min |
| 3000m | 48.0min |
| Payload | |
| Seats | 2 |
The first Soviet all-metal aircraft. It was built as a technology test platform. Pilot's open cockpit was located right behind the engine, above the wing leading edge. Two passengers were seated face-to-face in narrow toll fuselage of triangular section. Project started in May 1923.
Fuselage and wing frame was assembled of domestic aluminum alloy ('Kolchugaluminij') profiles. Skin - corrugated kolchugaluminij. Ailerons and elevators had rigid controls, rudder - wire controls.
Construction was very light, new design team (including A.I.Putilov, V.M.Petlyakov, I.I.Pogosskij, E.I.Pogosskij, N.S.Nekrasov, B.M.Kondorskij, A.I.Zimin et al) proved to be a serious competitor for Junkers (who dominated market of metal aircraft at the time).
First flight took place on May 26, 1923 (engineer N.I.Petrov). The only modification required was done quickly - slightly increase of the tailfin. Official acceptance trials in presence of deputies from UVVS and TsAGI - May 28, 1923.
There were still no domestic 100hp engine available, and passenger capacity was too small for mass use. ANT-2 remained a technology demonstrator, but first step to all metal monoplane concept was made.
| Predecessors | Modifications |
|---|---|
| - |
ANT-3 R-3 |
| References | |
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16k b/w ANT-2 drawing from "History of aircraft construction in the USSR", Vol.1 p.364; Used for background on this page. |
| Modified August 28, 1998 |
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