It's not the same with other self-launchers, of course, but my S10-VT
has a turbocharged, 4-cylinder engine rated at 115 (nominal)
horsepower. With the turbo, it achieves its rated power to a very high
altitude, which I haven't seen stated, but it has a published service
ceiling of 33,000' MSL. Density altitude has no effect on it other than
some reduction in propeller efficiency and engine temperature limits. I
imagine the higher true airspeed for a given IAS at takeoff at high
altitude airports makes up for reductions in wing lift. At maximum
power it burns around 5 gallons/hour (about 3.2 gph in cruise at 18,000'
MSL for repositioning flights), so I'd guess I burn less than a half
gallon of gas per normal soaring flight, including taxi and takeoff.
Engine overhaul will cost a few pennies more than with the smaller ships...
--
Dan, 5J