Traced the longeron and stringer holes from the temporary firewall to the permanent bottom half firewall and cut out the new holes. Trial fit the bottom permanent firewall at the rear of the fuselage. More adjustments required before floxing in place.
Aileron rolls and spins over the south shore of Rice Lake at 5000 ft. Click here for the video clip from the flight.
Click on the test headings for the video clips… The purpose of the Hyb-B test series is to develop a dependable ignition system for a hybrid rocket motor. Test Hyb-B-8 provided the best result and we’ll be moving to the next step of developing a hybrid rocket ignition system based on these results. Test Hyb-B-4 Setup …
Integrated Propulsion System Update – July 16, 2017 Read More »
Trimmed and sanded the 6-ply layup on the aft side of the forward landing gear bulkhead. Filed and sanded the 7/8″ holes for the aileron torque tubes to ensure good alignment. Placed the fuselage back on the saw horses and vacuumed the workshop.
