OH-1's powerplant XTS1-10 experimental type of production type TS-1-M-10.
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Turboshaft Engine Mitsubishi XTS-1-10 for OH-1
Ninja Scout Helicopter
2000 JGSDF Camp Tachikawa Airshow
OH-1's powerplant XTS1-10
experimental type of production type TS-1-M-10.
XTS1-10's poster description.
Compression ratio is 11.0 by
single-stage centrifugal compressor.
On this board
IRP : 940hp
MCP : 827hp
Acceleration and deceleration between IRP and FLY idle : 2 second
SFC
: 0.234kg/shp-hour
Turbine Inlet Temparature : 1170degC
Length : 1051mm
Width : 624mm
Height : 611mm
Weight : 157.85kg
Black box is the FADEC (Full
Authority Digital Engine Control)
Blown
part is IPS (Inlet Perticle Separater)
IRS
(Infra-Red Suppresser).
Experimental engine equips the straight-type
tail pipe.
White
box under IRS is oil cooler unit.
Exhaust
pipe.