Junkers K 16

Junkers K 16

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The Junkers K 16 was a small airliner produced in Germany in the early 1920s. It was a conventional, high-wing cantilever monoplane of all-metal construction, equipped with fixed, tailwheel undercarriage. The pilot sat in an open cockpit, while the two passengers were provided with an enclosed cabin within the fuselage. Shortly after the prototype flew, aircraft production in Germany was brought to a complete halt by the Allies, and the K 16 was quickly evacuated to the Netherlands to avoid confiscation. There, it was stored by Fokker until the restrictions were relaxed and work recommenced at Junkers' Dessau factory in 1924. By this time, however, the airline niche that the tiny K 16 had been intended to full no longer existed, and the small number that were produced were mostly sold to private owners. Junkers entered two K 16s in the 1925 Deutsche Rundflug, with one machine winning second place in the competition.

Variants

* K 16 - initial version with Siemens-Halske Sh 4 engine, later changed to Siemens-Halske Sh 5
** K 16a - modified undercarriage and rear fuselage (modified from prototype)
** K 16b - production versions with new wing and a variety of engine choices:
*** K 16ba - Siemens Sh 5 engine
*** K 16bi - Siemens Sh 20 engine
*** K 16bo - Walter NZ 120 engine
** K 16c - as K 16b but with modified nose section to accommodate engine change
*** K 16ce - Bristol Lucifer engine

pecifications (K 16 prototype)

aerospecs
ref=
met or eng?= met

crew=One pilot
capacity=2 passengers
length m=8.00
length ft=26
length in=3
span m=11.00
span ft=36
span in=1
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=2.75
height ft=9
height in=0
wing area sqm=16.50
wing area sqft=178
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
wing profile=
empty weight kg=430
empty weight lb=950
gross weight kg=850
gross weight lb=1,870
lift kg=
lift lb=

eng1 number=1
eng1 type=Siemens-Halske Sh 4
eng1 kw= 49
eng1 hp= 65
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=
eng2 lbf-ab=

max speed kmh=145
max speed mph=91
max speed mach=
cruise speed kmh=
cruise speed mph=
stall speed kmh=
stall speed mph=
range km=600
range miles=375
endurance h=
endurance min=
ceiling m=
ceiling ft=
g limits=
roll rate=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=
aircontent
see also=
related=
similar aircraft=
lists=

References

*
*
* [http://hugojunkers.pytalhost.com/ju_k16_a1.htm Hugo Junkers Homepage]
* [http://www.airwar.ru/enc/law1/juk16.html Уголок неба]


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