AERO Ae-45, Ae-145. 1952.Last change: February 2020
095b Section 1952-03-15
AERO Ae-45, Ae-145
Commercial and sanitary aircraft.
Construction Aero Ae-45
The Aero Ae-45 aircraft is a four-seater commercial and sanitary aircraft. All metal construction.
Double-girder flap, covered with dural steel sheet, equipped with crocodile flaps. There are slots between the engines and the fuselage that extend when the chassis is opened. The shuttlecocks are covered with canvas.
The fuselage is half-shell, covered with duralumin sheet.
Classical arrangement. Canvas covered rudders.
The aircraft landing gear is classic retractable in flight.
The Aero Ae-45 drive is two Walter "Minor 4 III" in-line engines with 2 x 107 HP nominal power (2 x 78 kW) and 2 x 80 HP (2 x 80 HP) throughput.
Aero Ae-145 drive is two Walter M-332 engines, 2 x 140 HP (2 x 103 kW). The engine is in-line, with hanging pistons, air-cooled.
Data T-T Aero Ae-45
Span of 12.25 m
Length 7.55 m
Height 2.35 m
Bearing area 17.09 m2
Curb weight 845 kg (Ae-45), 960 kg (Ae-145)
Payload 550 kg
Take-off weight 1,400 - 1,500 kg
Maximum speed 280 km / h
Cruise speed 245 km / h
Landing speed 90 km / h
Ceiling 4 700 - 5 900 m
Range 1,400 - 1,700 km
Written by Karol Placha Hetman