Integrated Propulsion System Update – May 7, 2017
For upcoming hybrid rocket testing (Hyb-A-1), the paraffin rocket motor was secured to a test stand using two clamps and the nitrous oxide cartridge was weighed prior to the test.
For upcoming hybrid rocket testing (Hyb-A-1), the paraffin rocket motor was secured to a test stand using two clamps and the nitrous oxide cartridge was weighed prior to the test.
A 0.25″ diameter, 12″ long drill bit was inserted through the existing holes in the forward landing gear bulkhead and, using the inside plywood corners as guides, 0.25″ holes were drilled through the hard points in the aft bulkhead. The 8″ x 8″ squares were knocked out and glue scraped off of the bulkheads.