How does the Raptor fly compared to regular flex wings?
The Raptor has a very responsive control system combined with a fast roll rate. Most pilots over controled at first until realizing how little effort is needed. Flex wing pilots who made there first flight on the Raptor had little problem adapting.
What's the difference between the Raptor and other rigid wings?
Most rigids I have seen use spoiler controls and have a flap. The flap is made possible by sweeping and twisting the wing. This added pitch stability at the tips offsets the pitch instability created by deploying flap. This as an elegant solution. It gives a thick slow speed airfoil for slow flight and a thinner airfoil for high speed flight.
The Raptor takes a different approach. Use a pitch stable airfoil over the entire wing. Reduce sweep and twist to a minimum. What's the minimum? For twist it's the least required to prevent tip stalls. Twist hurts high speed performance.
For sweep that's where it gets interesting. Jim Marskes wings have shown pitch stability is possible using the right airfoil. Sweep isn't necessary for pitch stability however a wing without sweep has very little directional stability requiring a large rudder. Also on a wing with no sweep the hook in point for the pilot differs greatly from where the empty balance point on the wing alone. Why does this matter? Because the pilot is hanging from the wing not firmly attached. If the pilot encounters negative G load and the hang strap goes slack The wing alone would be unstable.
So the design philosophy of the Raptor was to use a tapered D-tube to reduce needed sweep. Then set the sweep so the hook in point converges with the balance point of the empty glider. The sweep isn't high enough for good directional stability so Tip rudders supplement it.
What materials are used in Raptor construction?
Raptors use Graphlite rods for spars and high stress areas. The D-tubes do not use core material and are solid composite laminates. D-tubes have been made from fiberglass, carbon fiber and Kevlar and various combinations. Kevlar seems the best suited material for D-tubes.
Ribs are combination of wood cap strips bonded to a composite panel. Hard wings use wood trailing edge. Collapsible wings use standard sailcloth. Ribs use the same construction as hard wing but with additional reinforcements added.
Is the Raptor certified ?
The Raptor is not certified by the HGMA. There are no plans to certify it at this time.
How do you load test wings?
The wing is suspended or supported upside down for positive load test. Then weight is added to simulate flight loads. Raptors are tested for positive and negative 5G @ 300lb hook in. Therefore 1500 lbs of weight is added to wing across the span. I usually test the D-tubes alone since they are the main structural component. The load test of the Cantilever R2r. With no load.
Full load. Willie is pushing down on tip until other tip is airborne.
Is there a tail available for the Raptor?
There are no plans to add a horizontal tail to the Raptor. It doesn't need one. It is recommended that a keel fin be used for additional direction stability.
Has the Raptor been spin tested? How easy does it spin?
I was able to push the R1 into a spin by first stalling in in a moderate turn then denying recovery from stall. Basically when the stall hits the nose will drop and glider will recover. If you keep pushing out and deny the recovery and push it far enough it will spin. I never let the spin fully develop and didn't rotate more than half turn. The recovery was easy let bar return to trim and apply opposite rudder. Easy but scary. The glider would pitch nose down and pick up speed fast. Once the reflex kicked in it would level out. The scary thing was it could use up 200 to 300' of altitude in the blink of an eye.
There has been one accidental spin in the Raptor. It happened during a test flight on the second R1. Shortly after launching on an air tow I discovered my hang point was way off. To maintain flying speed required a lot of back pressure on the control bar. I was eager to test this wing so decided to tow to altitude 3000' anyway. The tow went fine. I was able to test roll stability and turn reversals on wing. Everything felt fine except for problem with trim speed. After driving around for a while to loose altitude I made a high banked 180 to line up with landing field. I also did something incredibly stupid. I let the bar go out to trim. It felt like the glider flared to a stop while banked 45 degrees. When I realized what I done it was too late The glider already entered a spin. I only had about 100' not enough room to recover. I had spun tested 1/4 scale models of the Raptor and they spun flat and fast like a maple seed. So I decided to push out even more. The theory was the faster I spun The slower the descent rate. The result is I got three complete revolutions in before impact. I suffered a broken wrist and spent a few nights in the hospital. Did the theory of spin faster pay off? I don't know but did learn one very important lesson. Do not fly a glider if the trim speed isn't set right land it and fix it.