Regarding the power requirements - I had this rule of thumb ferreted away in my files;
A Diesel Engine produces about 20lb of thrust per horsepower
In the case of the M25 in an O'day 34/35, 21hp= 420lbs of thrust @ 3000RPM
" Detail; the very approximate calculation goes like this:
Take the engine power in Watts. If it is given in HP, then multiply by 746 to obtain the power in Watts. Call this power BSP (brake shaft power).
Multiply BSP by transmission and propeller efficiencies. You can assume around 0.5 as a maximum total efficiency of such a small prop. Call this power PE (effective power).
Convert the speed to meters per second (m/s). To do that, multiply the speed in knots by 0.514 . Then multiply again by 0.95, to approximately take into account the eventual effect of the hull wake. Call this speed Vp.
To obtain thrust given by the prop, divide PE by Vp: T = PE / Vp .
This will be the available thrust in Newtons, for that speed and engine power. I'm using all SI units, to avoid errors related to inconsistent units. To convert this thrust to lbs, multiply by 0.225 .
That's all.
If you think you'll need to do more such calculations in future, and/or have them more precise, I suggest you buy the excellent Dave Gerr's book "The Propeller Handbook". You can find it at Amazon for $12, a real bargain for the knowledge it contains:
http://www.amazon.com/gp/offer-listi...condition=used"