Jordi Grau
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- Joined
- Oct 9, 2018
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Hi all, I'm an student doing its final degree project in aerospace engineering. My project is to design a nozzle for the rocket that we do in our university, I have been gathering information but I can't seem to find the following:
Regarding Aerotech engines:
- Which composition is the Redline propellant made off? With the general composition I'm fine.
- As I'm starting my iterative design on an I600R engine, for a program that I use to calculate thrust curves I need the throat diameter as well as the most exterior diameter of the nozzle divergent part. I can't find any drawing or plan with the dimentions in it.
Thank you very much for any help that you can give me.
Regarding Aerotech engines:
- Which composition is the Redline propellant made off? With the general composition I'm fine.
- As I'm starting my iterative design on an I600R engine, for a program that I use to calculate thrust curves I need the throat diameter as well as the most exterior diameter of the nozzle divergent part. I can't find any drawing or plan with the dimentions in it.
Thank you very much for any help that you can give me.