词条 | Aero L-60 Brigadýr | ||||||||||||||||
释义 |
The Aero L-60 Brigadýr ({{lang-cs|Brigadier}}) was a small, high-wing propeller-driven Czechoslovakian STOL utility aircraft developed for both civil and military use. A prototype, designated XL-60, with Argus As 10C engine, first flew on December 24, 1953, but it was not successful. The plane was thoroughly redesigned and the second improved prototype, with M-208B flat-six engine, flew on June 8, 1954. The aircraft's configuration bears a strong resemblance to the Fieseler Fi 156 "Storch" licence-produced in Czechoslovakia during and after World War II (as K-65 Čáp), and which this aircraft was intended to replace. By the end of production in 1960, 273 had been built by Aero, including an improved version, the L-160 with an all-metal tail. Aircraft retrofitted with a PZL-built Ivchenko AI-14R radial engine are known as the L-60S. Variants
OperatorsCivil operators[1]
Military operators
Specifications (L-60){{aircraft specifications|plane or copter?= plane |jet or prop?= prop |ref=Jane's All The World's Aircraft 1961–62[3] |crew= One, pilot |capacity=Three passengers |length main= 8.54 m |length alt= 28 ft 0 in |span main= 13.96 m |span alt= 45 ft 9½ in |height main= 2.72 m |height alt= 8 ft 11 in |area main=24.30 m² |area alt= 261.6 ft² |airfoil=NACA 4412 |aspect ratio=8.07:1 |empty weight main=968 kg |empty weight alt= 2,134 lb |loaded weight main= 1,460 kg |loaded weight alt=3,219 lb |useful load main= |useful load alt= |max takeoff weight main= 1,560 kg |max takeoff weight alt= 3,439 lb |more general= |engine (prop)=Praga Doris M 208-B |type of prop=air-cooled flat-six |number of props=1 |power main= 142 kW |power alt= 190 hp |power original= |max speed main= 193 km/h |max speed alt= 104 knots, 120 mph |cruise speed main= 175 km/h |cruise speed alt= 95 knots, 109 mph |cruise speed more=at sea level |never exceed speed main= |never exceed speed alt= |stall speed main= 52 km/h |stall speed alt= 28 knots, 32 mph |range main= 720 km |range alt= 389 nm, 447 miles |ceiling main= 4,200 m |ceiling alt= 13,780 ft |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance=*Climb to 1,000 m (3,300 ft): 4.3 min |armament= |avionics= }} See also{{aircontent||related= |similar aircraft=
|lists= |see also= }} References
1. ^Krzyżan, Marian, Samoloty w muzeach polskich, Warsaw: Wydawnictwa Komunikacji i Łączności, 1983, {{ISBN|978-83-206-0432-0}} 2. ^Moldova György: Égi szekér, Magvető Könyvkiadó, 1982, {{ISBN|963-271-750-3}} 3. ^Taylor 1961, p. 35.
External links{{Commons category|Aero L-60 Brigadýr}}
7 : Aero Vodochody aircraft|Czechoslovakian civil utility aircraft 1950–1959|Czechoslovakian military utility aircraft 1950–1959|Glider tugs|Single-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1953 |
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