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This is a great resource. Thanks from RHIT's Rocketry Club!
Agreed
These have been very informative, thank you for posting.
Hi. I really could use your help with an equation used to calculate the combustion chamber size for a rocket powered by Methalox.
its an old post BUT...arent the units a bit messed up ?And...(1.27) * (3.004 * 10^-4) = ???
Why did you choose 1000psi and how to calculate the real pressure of combustion pressure?
Is it possible to get that matlab code? It would be a super useful tool for my club!
Is there a link available for this presentation?
A bit late bute here is the link for the presentation: static1.squarespace.com/static/5c639f2e11f78440d05623e3/t/5c6b9076e2c48352e13fa8ab/1550553213416/LCCLS+Rocket+Engine+Sizing+compressed.pdf
@@emanuelsantos4252 thank you
This is a great resource. Thanks from RHIT's Rocketry Club!
Agreed
These have been very informative, thank you for posting.
Hi. I really could use your help with an equation used to calculate the combustion chamber size for a rocket powered by Methalox.
its an old post BUT...
arent the units a bit messed up ?
And...
(1.27) * (3.004 * 10^-4) = ???
Why did you choose 1000psi and how to calculate the real pressure of combustion pressure?
Is it possible to get that matlab code? It would be a super useful tool for my club!
Is there a link available for this presentation?
A bit late bute here is the link for the presentation: static1.squarespace.com/static/5c639f2e11f78440d05623e3/t/5c6b9076e2c48352e13fa8ab/1550553213416/LCCLS+Rocket+Engine+Sizing+compressed.pdf
@@emanuelsantos4252 thank you