ANT-5 prototype and pre-production I-4 by P.O.Sukhoj/ A.N.TupolevA ll-metal sesquiplane fighter, with small cantilever lower wing. The order for this fighter
was issued in Fall 1925 by TsAGI.
Comparison of all-metal vs mixed vs wooden construction fighter was the key idea. General construction of the ANT-5 was similar
to this of ANT-2 and ANT-3/R-3.
Prototype had to be powered by single 420/525hp Jupiter-VI, which has to be
replaced by more powerful domestic M-22 on series aircraft.
| Technical data | |||||||
|---|---|---|---|---|---|---|---|---|
| Type | ANT-5 | I-4 'Dubler' | I-4 Pre-series | |||||
| Function | Prototypes | Pre-production | ||||||
| Year | 1927 | 1928 | 1928 | |||||
| Crew | 1 | 1 | 1 | |||||
| Engines | 1*420/525hp Gnome-Rhone Jupiter-VI | 1*480hp M-22 | ||||||
| Length | 7.28m | |||||||
| Wingspan | 11.4m | |||||||
| Wing area | 23.8m2 | |||||||
| Empty weight | 921kg | 941kg | 974kg | |||||
| Loaded weight | 1343kg | 1363kg | 1426kg | |||||
| Wing load | 56.5kg/m2 | 57.3kg/m2 | 60.0kg/m2 | |||||
| Power load | 3.25kg/hp | 3.05kg/hp | 2.97kg/hp | |||||
| Speed at 0m | 246km/h | 257km/h | 247km/h | |||||
| Speed at 3000m | 250km/h | 250km/h | ? | |||||
| Takeoff Roll | 70m 6sec | 70m 6sec | 8sec | |||||
| Landing Roll | 140m 17sec | 140m 17sec | 19sec | |||||
| Turn time | - | 11sec | 12sec | |||||
| Range | - | 840km | - | |||||
| Flight Endurance | 2h18min | |||||||
| Ceiling | 8200m | 7650m | 7120m | |||||
| Climb | ||||||||
| 1000m | - | 1.8min | ||||||
| 2000m | - | 4.1min | ||||||
| 3000m | - | 6.7min | ||||||
| 5000m | 11.4min | 11.0min | 12.4min | |||||
| Payload | ||||||||
| Fuel+Oil | 236+25kg | |||||||
| Armament | ||||||||
| Guns | 2*mg7.62mm | |||||||
| Created January 25, 1996
Modified March 03, 1998 by Alexandre Savine |
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