I didnt even intend links, just copy pasted the article, and it is
such a COOL history, I thought I'd post it.

The revolutionary takeaways were:

small size
novel construction
very high strength
inexpensive across the board
retracts!
speed and performance as well as economy

The later areas for improvement:

dynel cracking (easy update new projects to fiberglass)
vw bug engine reliability (cracks crank, heads, seems usually resolved)
landing gear bolt breakage (easy fix)


just a few random memories from decades ago, it seems co-developer stu
robinson kept a low profile.  also RR developed 3-blade ground
adjustable composite props that developed cracking at the base of the
blade. But a VERY cool look!  I'd like to have 3 blades for looks and
ground clearance if I ever get my project off the ground, and
tri-retracts since I dont have tailwheel time.

oh and people questioned the strength of the WAF's until it became
abundantly apparent they simply do not fail!

the few turbo projects were really performing well. IIRC they used
small normalizing rayjay turbocharger, but these I think exacerbated
the vw issues.

I am looking possibly at d-motor for mine, and wonder if a light
normalizing turbo option could apply...









> That link should read
> http://aerofoilengineering.com/KR/sportaviation/Kr73-1.HTM   .
>

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