ANT-35, ANT-35bis, PS-35 by A.A.Arhangelsky and A.N.Tupolev
P assenger version of the SB high speed bomber.
Aircraft was built in parallel with SB production steaming up, and faced no serious
drawbacks. It used wing, tail and landing gear of the bomber. New fuselage provided room for ten seats, buffet, lavatory and
luggage section. Excellent sound insulation, common and individual ventilation, heating system provided passenger with world
class comfort, while rich cockpit equipment (including autopilot) guaranteed safe flights.
| Technical data | |||
|---|---|---|---|---|
| Type | ANT-35 | ANT-35bis PS-35 | ||
| Function | Passenger Prototype | Passenger | ||
| Year | 1936 | 1937-39 | ||
| Crew | 2 | |||
| Engines | 2*800hp M-85 | 2*1000/840hp M-62IR | ||
| Length | 14.95m | 15.4m | ||
| Wingspan | 20.8m | 20.8m | ||
| Wing area | 57.8m2 | 57.8m2 | ||
| Empty weight | 4710kg | 5012kg | ||
| Loaded weight | 6620kg | 7000kg | ||
| Wing load | 114kg/m2 | 121kg/m2 | ||
| Power load | 4.1kg/hp | 3.3kg/hp | ||
| Speed at 0m | 350km/h | 350km/h | ||
| Speed | 400km/h at 4000m |
372km/h at 1500m | ||
| Landing Speed | 95km/h | 105km/h | ||
| Landing Roll | - | 19sec 300m | ||
| Takeoff Roll | - | 10sec 225m | ||
| Range | 1200-2000km | 1640km | ||
| Flight Endurance | 5h | 5h | ||
| Ceiling | 8500m | 7200m | ||
| Climb | ||||
| 3000m | - | 6.1min | ||
| 5000m | - | 13min | ||
| Payload | ||||
| Seats | 10 | 10 | ||
| Load | 840kg | 840kg | ||
| Modified February 05, 1998
by Alexandre Savine and Sergey Andreev; |
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