Kellett XR-10

Kellett XR-10

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The Kellett XR-10 was a military transport helicopter developed in the United States in the 1940s but which only flew in prototype form. It was designed in response to a USAAF Technical Instruction issued for the development of a helicopter to transport passengers, cargo, or wounded personnel within an enclosed fuselage. Kellett's proposal followed the general layout that the company was developing in the XR-8, with twin intermeshing rotors, and was accepted by the Air Force on 16 October over proposals by Sikorsky, Bell, and Platt-LePage.

The XR-10 resembled a scaled-up XR-8, although its twin engines were carried in nacelles at the fuselage sides, driving the rotors via long driveshafts, and the aircraft was skinned entirely in metal. The first of two prototypes flew on 24 April 1947, and at the time, was the largest rotorcraft to fly in the United States [NASM] . During test-flights, however, the same problem that had been encountered with the XR-8's rotor system emerged when blades from the two rotors collided in flight. With fixes in place, flight testing continued, but on 3 October 1949, the first prototype crashed due to a control system failure and killed Kellett's chief test pilot, Dave Driskill. The project was abandoned shortly thereafter, and a 16-seat civil variant, the KH-2, never left the drawing board.

pecifications

aerospecs
ref=
met or eng?= eng

crew=Two pilots
capacity=10 troops "or" 6 stretchers "or" 3,550 lb (1,610 kg) of cargo
length m=8.89
length ft=29
length in=2
span m=
span ft=
span in=
swept m=
swept ft=
swept in=
rot number= 2
rot dia m= 21.64
rot dia ft= 71
rot dia in= 0
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=4,340
empty weight lb=9,550
gross weight kg=6,990
gross weight lb=15,380
lift kg=
lift lb=

eng1 number=2
eng1 type=Continental R-975-15
eng1 kw= 317
eng1 hp= 425
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=160
max speed mph=100
max speed mach=
cruise speed kmh=
cruise speed mph=
stall speed kmh=
stall speed mph=
range km=560
range miles=350
endurance h=
endurance min=
ceiling m=4,600
ceiling ft=15,000
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

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* [http://aerofiles.com/_kellett.html aerofiles.com]
* [http://collections.nasm.si.edu/code/emuseum.asp?style=browse&currentrecord=1&page=search&profile=objects&searchdesc=kellett&quicksearch=kellett&newvalues=1&newstyle=single&newcurrentrecord=6 NASM website]


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