This 650 HP turbo p-port time to climb aircraft engine
certifies the Racing Beat aluminium end and centre housings
IMHO.

This engine, with turbo and gear box, is about 210 pounds
plus or minus 20.

That is a power to weight ratio of 3:1 in gas turbine
country with half the fuel burn. It would have more
power than a 650 HP gas turbine at over 20,000 feet.

The bare engine, with out the turbo or gear box, is 110
pounds roughly.


This would make a world beater installed in a Questair Venture
or Nemesis Next aircraft at Reno in the Sport Class.

Imagine a three or four rotor version of this engine.

Mazda is sitting on a gold mine and they don't know it.

Peter G, now at SZP with aircraft it is going in.

Paul Lamar

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