New member has questions`
Thread Starter
Can Post Only in New Member Section
Joined: Dec 2009
Posts: 3
Likes: 0
From: Lincoln,NE
Hello I'm Dave Zichek and I became a member to pick your brains about the Mazda rotary engine, which to me appears to be a compact robust and powerful engine I plan on using in my experimental Mustang II aircraft.
http://www.rotaryaviation.com/engine_products.htm
Normally aspirated, you can easily get around that 300 crank HP level from a 3 rotor / 20B.
why not 13b?
It would be a lot easier to find a 13b for cheaper and be able to get the parts and power out of it than the 12a, but I'm not sure what the limitations are for an aircraft engine.
Trending Topics
Thread Starter
Can Post Only in New Member Section
Joined: Dec 2009
Posts: 3
Likes: 0
From: Lincoln,NE
12A/13B for experimental AC
The biggest concern is weight that is why a 12A or 13B turbo is appealing you can get the power of a Lycoming IO 540 with the weight of an IO 360 by the way what would be the typical rpm of a 12A/13B twin turbo producing 300HP?
thanks Dave Z
thanks Dave Z
Thread
Thread Starter
Forum
Replies
Last Post






