I was looking over the work done by amateurs on peroxide/kero rocket
motors.
What I see so far is a lot of unstable motors with asymmetrical issues.
What I need is some good data and guidance working on a 1000-2000lb
range motor.
Time is a factor I need to be as close as I can to a working engine by
April.
Chamber pressure is ultimately 1000 psi
This is a test engine water cooled static test only.
I need tips and pitfalls from experienced rocketeers.