Since the recent posts by Charles E. Rogers (aka Crazy-Chuck) made several claims, I wanted to start an actual tech thread on those subjects.
- FAA approvals for sub-orbital rockets over 62 miles. a. What are the actual minimal requirements? b. What are the links to the regs as they stand post-change?
- Erosivity, starting with the exact grain geometry of the CSXT (future legend) rocket. a. Propellant burning rate and density (average at specified operating pressure) b. Propellant burning rate exponent.
- Governmental interfaces other than FAA required to achieve the flight (FCC, EPA, BLM, etc).
Tech Jerry