- Atlas H-10
__NOTOC__ Infobox Aircraft
name=H-10
caption=
type=Civil utility aircraft
manufacturer=Atlas Aircraft
designer=Max Harlow
first flight=1948
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Atlas H-10 was a prototype for a four-seat cabinmonoplane aircraft flown in theUnited States shortly afterWorld War II . It had been constructed from the unfinishedHarlow PJC-4 sportingbiplane abandoned at the outbreak of the conflict.It was a low-wing
cantilever monoplane of conventional configuration with retractable tailwheel undercarriage and powered by a variety of engines throughout its life. Originally powered by a Lycoming O-435, it was re-engined with two Continental O-300s driving contra-rotatingpropeller s through a common gearbox. In turn, this arrangement was replaced with a Franklin 6AB and finally a Lycoming IO-720.As of 2006, the aircraft was reportedly still in existence in a dismantled state in the hands of a
California n collector.pecifications (with Continental engines)
aerospecs
met or eng?= engcrew=one pilot
capacity=three passengers
length m=8.64
length ft=28
length in=4
span m=10.90
span ft=35
span in=9
dia m=
dia ft=
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height m=
height ft=
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wing area sqm=
wing area sqft=
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=
gross weight lb=eng1 number=2
eng1 type=Continental O-300
eng1 kw= 108
eng1 hp= 145
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=274
max speed mph=170
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
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armament6=References
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* [http://www.aerofiles.com/_al.html aerofiles.com]ee also
aircontent
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