Red Baron 2

 

Rollout and First Flight

During the first engine run, flames from the stacks were perfect, even with ADI on and off, throttle ups and downs and rapid throttle bursts.

Test flying revealed a problem with stability. The tail area was increased. Years later test pilot Darryl Greenamyer identified an aft CG condition that was corrected by moving the battery forward about six feet.

While the contra-rotating propeller produces less torque reaction, it also chops up the air more, requiring larger vertical surfaces to compensate.

Nearing Completion

Nearing Completion

Nearing Completion

Nearing Completion

Nearing Completion

Rollout. Jerry Morrison on Wing

Rollout

Engine Runup. Dave Zeuschel at the Controls

After Engine Runup

Dave Zeuschel Inspects Engine After Runup

Bob Carr, RC Richardson, Jerry Morrison, Robbie Patterson, Mac McLain in Cockpit

RC Richardson, Randy Scoville, Doug Kruse

Engineering: Pete Law, Bruce Boland

Ready for Flight

It Flys! Later Image Showing Re-Worked Vertical Tail.

 

1975 Camapign

In an attempt to improve stability the crew hastily added a ventral fin. The ventral fin was eventually removed once the tail was enlarged and CG problems solved.

Mojave

Mojave

Mojave

Mojave

Mojave: Randy Scoville, John Muszala, Robbie Patterson

Mojave: Pete Law

Mojave

Mojave

Mojave

Mac McClain - Pilot

Mojave: Note Quickly-Added Ventral Fin

September, at Home. Note Re-Worked Vertical Tail

Reno

Reno

Reno

 

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Home Up Red Baron 3

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