“DINFIA IA 45”的意思、由来-开放百科全书

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DINFIA IA 45

释义

Development
Variants
Specifications (IA 45B)
References

name=IA 45 Querandi

image=I.Ae. 45 Querandí.jpg

caption=
}}{{Infobox Aircraft Type

type=Light transport

manufacturer=DINFIA

national origin=Argentina

designer=

first flight=1957

introduced=

retired=

status=

primary user=

more users=

produced=

number built=2

variants with their own articles=
}}

The DINFIA IA 45 Querandi was a 1950s Argentine twin-engined light transport aircraft built by the DINFIA.

Development

The IA 45 Querandi was designed as an executive and light transport. A twin-engined all metal high-wing cantilever monoplane with an upswept rear fuselage, it had a tailplane with two fins and rudders and retractable tricycle landing gear. Powered by two pusher configuration Avco Lycoming O-320 piston engines it had room for a pilot and four passengers. The prototype first flew on 23 September 1957 and was followed by an improved version with more powerful engines and six seats.

Variants

IA 45

Prototype powered by two Avco Lycoming O-320 piston engines, one built, first flight 23 September 1957.

IA 45B

Improved version with six seats and powered by two Lycoming O-360 piston engines, one built, first flight 15 November 1960.

Specifications (IA 45B)

{{aerospecs
|ref=Jane's All The World's Aircraft 1961–62^[1]
|met or eng?=met
|crew=one
|capacity=five passengers
|length m=8.92
|length ft=29
|length in=3
|span m=13.75
|span ft=45
|span in=2
|height m=2.79
|height ft=9
|height in=2
|wing area sqm=19.3
|wing area sqft=207.7
|aspect ratio=9.8:1
|airfoil=NACA 23016 at root, 23010 at tip
|empty weight kg=1170
|empty weight lb=2579
|gross weight kg=1800
|gross weight lb=3968
|eng1 number=2
|eng1 type=Lycoming O-360 flat-four piston engine
|eng1 kw=134
|eng1 hp=180
|eng1 kn=
|eng1 lbf=
|max speed kmh=275
|max speed mph=171
|max speed mach=
|cruise speed kmh=245
|cruise speed mph=152
|range km=1,100
|range miles=680
|endurance h=
|endurance min=
|ceiling m=7,500
|ceiling ft=24,600
|glide ratio=
|climb rate ms=7.0
|climb rate ftmin=1,380
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}

References

Notes

1. ^Taylor 1961, p. 4.

Bibliography

The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing
Taylor, John W. R. Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company, 1961.

4 : Argentine civil utility aircraft 1950–1959|FMA aircraft|Twin-engined pusher aircraft|High-wing aircraft

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