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- Aug 1, 2014
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Still working on design and developing questions with potential solutions for a 2-stage project. Trying to anticipate problems and how to avoid them. While I have found a few 2-stage kits out there, I’m strongly leaning for scratch build. I will try to incorporate error proofing designs to minimize mistakes. All of my rockets are numbered and I keep track of all flights in a spreadsheet. This rocket will be number 100 in the fleet that I’ve built over the decades from mod rocs to HP.
So my questions now are on the separation charge vs just relying on drag separation. I’ve found here that people use about 0.5 gms 4F (I will ground test when built.). Anyway, I assume the charge is placed at the top of the ISC and controlled from the ISC “fired” via another timer. What are your design attributes to minimize fouling the ignitor and motor in the sustainer? Other words of wisdom? Thanks!!!
So my questions now are on the separation charge vs just relying on drag separation. I’ve found here that people use about 0.5 gms 4F (I will ground test when built.). Anyway, I assume the charge is placed at the top of the ISC and controlled from the ISC “fired” via another timer. What are your design attributes to minimize fouling the ignitor and motor in the sustainer? Other words of wisdom? Thanks!!!