Gotha Go 146

__NOTOC__ Infobox Aircraft
name=Go 146


caption=
type=Utility aircraft
national origin=Germany
manufacturer=Gotha
designer=Albert Kalkert
first flight=avyear|1936
introduced=
retired=
status=
primary user=
more users=
produced=
number built=ca. 4
variants with their own articles=The Gotha Go 146 was a twin-engine utility aircraft developed in Germany in the mid-1930s. It was a conventional low-wing cantilever monoplane with tailwheel undercarriage, the main units of which retracted into the engine nacelles on the wings. It was offered to the Luftwaffe as a high-speed courier aircraft, but the Siebel Fh 104 was selected instead. With Gotha unable to attract other customers, no serious production was undertaken and a small number of prototypes were the only examples built.

pecifications

aerospecs
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met or eng?= met

crew=One pilot
capacity=4 passengers
length m=9.45
length ft=31
length in=0
span m=12.40
span ft=40
span in=8
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=2.70
height ft=8
height in=10
wing area sqm=21.7
wing area sqft=234
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=1,520
empty weight lb=3,350
gross weight kg=2,200
gross weight lb=4,850
lift kg=
lift lb=

eng1 number=2
eng1 type=Hirth HM 508E
eng1 kw= 180
eng1 hp= 240
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=335
max speed mph=208
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,000
range miles=620
endurance h=
endurance min=
ceiling m=5,000
ceiling ft=16,400
glide ratio=
climb rate ms=7.5
climb rate ftmin=1,470
sink rate ms=
sink rate ftmin=

armament1=
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armament5=
armament6= aircontent
see also=
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References

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