Setup and initial testing of our remotely controlled ignition system. Here is a video of the workshop tests. The ignition system prototype is now being prepared for outside tests at our Crooked Creek Facility.
The team met in the Cobourg workshop to progress the planning and design efforts for our integrated propulsion system development program.
Checking out if a National 490-C parachute will fit well in the front of the Citabria. Unfortunately it positions the front pilot too close to the instrument panel. The parachute should work ok for the rear pilot/passenger though. Will check it out next flight opportunity. Gave the engine a run and uncovered a problem with …
Setup for Test Hyb-C A small hole was drilled into the combustion chamber side of the cylinder. Wires for the spark gap igniter were inserted through the hole and into the cylinder. Paraffin was melted and poured into the cylinder and black powder was applied to the paraffin on the combustion chamber side. A small …
Integrated Propulsion System Update – August 6, 2017 Read More »
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 »
