George Toth from Texas built one many years ago.

Bob Sauer
Sun City West, Az
N811RJ Flying

On Sun, Dec 12, 2021 at 5:08 AM Craig Williams <cr...@kr2seafury.com> wrote:

> I think there's a reason you only see one Vans model that's a 4-seater.
> Not a big market and there are plenty of 4 seat options out there already.
> IMO a 4 seater KR would be a waste of someones time unless you just like
> building one off airplanes.
>
>
> CRaig
> N886MJ (N51CW)
> N6423B
>
>
>
>
> > On 12/12/2021 2:51 AM Samuel Spanovich <spanovich...@gmail.com> wrote:
> >
> >
> > I’ve seen online that a small group of designers have started the
> “KR-Super 2” design, however has anyone out there ever started a 4-seater
> KR design?
> >
> > With the price of 4-seater airplanes these days being well into the
> 6-figure regime, I would think a KR4 would be a very popular design for
> those who just want an extra seat or two for the occasional passenger, or
> just a little extra luggage space.
> >
> > Most KR2S’s have an empty weight of around 600-700 lbs (mine is 650)
> with a Revmaster 2100 (65 HP), and a gross weight of approximately
> 1000-1200 lbs (mine is 1150 lbs).  This offers fairly decent performance;
> not great, but not terrible either.
> >
> > If this “KR4” were to be powered by a 100 HP Continental O-200, in
> theory,  to achieve the same Power/Weight ratio as the Revmaster, you could
> have a gross weight of approximately 1750 lbs. For a little factor of
> safety, let’s assume a Gross Weight of 1650 lbs.
> >
> > Of course when talking about a bigger airplane, you would need a bigger
> engine, a bigger structure, which means more weight.
> >
> > Base Empty Weight = 650 lbs
> > Engine Increase (2100D to O-200) = +50 lbs
> > Structural Increase (bigger airplane)  = +250 lbs
> >
> > KR4 Empty Weight ~ 950 lbs
> > Gross Weight = 1650
> >
> > That leaves 700 lbs for fuel, passengers, and luggage. For a Continental
> 0-200, you could plan on about 6 gallons per hour, and could use 22 gallons
> for about 3 hours of endurance with a 30-45 minute reserve. This would
> leave you with 568 lbs for passengers/luggage. This would be plenty for two
> passengers and a lot of luggage, or three medium sized passengers and a
> small amount of luggage, or three larger (190 lb passengers) with no
> luggage.
> >
> > If you managed to get 100-110 knots with this setup you would have a
> range of about 300-330 NM.
> >
> > So what do you guys this?  For those that have experience building, what
> limitations would there be with widening the structure, lengthening the
> fuselage, and also increasing the wing surface area?  Would it be a matter
> of just building a stronger/thicker spar/wing, or is there more to this
> than I am realizing?
> >
> > I should have prefaced this with I am not an aircraft designer.
> >
> > Very Respectfully.
> >
> > Sam Spanovich
> > N6399U
> > 74S, Anacortes WA
> >
> >
> > Sent from my iPhone
> > ________________________________
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