Antonov A-13

__NOTOC__ Infobox Aircraft
name=A-13


caption=
type=Sailplane
manufacturer=Antonov
designer=
first flight=1958
introduced=
retired=
status=
primary user=
more users=
produced=
number built=~200
variants with their own articles=The Antonov A-13 was a Soviet aerobatic sailplane flown in the 1950s and 60s. It was a small, single-seat, all-metal aircraft developed from the A-11 and which could optionally be fitted with that aircraft's longer-span wings. It was a mid-wing monoplane with a tadpole-like fuselage and a V-tail. In February 1962, an A-13 was fitted with a small turbojet engine to set a world airspeed record of 196 km/h (122 mph) for an aircraft up to 500 kg. This jet-powered version is known as the An-13

Variants

* A-13 : Single-seat aerobatic sailplane.
* A-13M : Motor glider version, fitted with a low-powered piston engine.
* An-13 : Jet-powered version.

pecifications (A-13)

aerospecs
met or eng?= met

crew=one, pilot
capacity=
length m=6.4
length ft=21
length in=0
span m=12.1
span ft=39
span in=8
dia m=
dia ft=
dia in=
height m=1.6
height ft=5
height in=3
wing area sqm=10.4
wing area sqft=112
rot area sqm=
rot area sqft=
aspect ratio= 14:1
empty weight kg=270
empty weight lb=600
gross weight kg=360
gross weight lb=800

eng1 number=
eng1 type=
eng1 kw=
eng1 hp=
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
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max speed kmh=400
max speed mph=250
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio= 25:1
climb rate ms=
climb rate ftmin=
sink rate ms= 1.1
sink rate ftmin= 220

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