Kraft Super Fli

__NOTOC__

The Kraft K-1 Super Fli was a single-seat sport aircraft designed in the United States in the early 1970s and marketed for homebuilding. It was a low-wing cantilever monoplane of conventional design with fixed, tailwheel undercarriage. The wings had a wooden structure, skinned in plywood, while the fuselage and empennage were built from steel tube, the fuselage skinned in aluminium and the tail in fabric. It had a very similar design to radio controlled craft.

The Super Fli's designer, Phil Kraft, was a champion builder and flier of radio-controlled model aircraft who in 1972 decided to apply this expertise to the design of a full-size aircraft. The design was therefore based around the guidelines normally applied to model aircraft, particularly in in its wing design, areas, and moments.

pecifications

aerospecs
ref=
met or eng?= eng

crew=One pilot
capacity=
length m=
length ft=
length in=
span m=7.32
span ft=24
span in=0
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=
height ft=
height in=
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
wing profile=
empty weight kg=445
empty weight lb=980
gross weight kg=635
gross weight lb=1,400
lift kg=
lift lb=

eng1 number=1
eng1 type=Lycoming IO-360-A1D
eng1 kw= 150
eng1 hp= 200
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=322
max speed mph=200
max speed mach=
cruise speed kmh=
cruise speed mph=
stall speed kmh=
stall speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=3,660
ceiling ft=12,000
g limits=
roll rate=
glide ratio=
climb rate ms=15.2
climb rate ftmin=3,000
sink rate ms=
sink rate ftmin=

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

References

*
*