Liquid rocket engine injector plate - Manufaturing, assembly and cold flow testing

Reodor is a liquid oxygen - liquid ethanol rocket engine developed by Portal Space.
Design Specifications:
Thrust: 3500 N
Mass Flow Rate: 1.47 kg/s
Specific Impulse: 245 s
Oxidizer - Fuel Ratio: 1.33
Combustion Chamber Pressure: 20 bar
Test specifications at hot fire:
Average Thrust: ~2400N
Average Chamber Pressure: ~19 bar

[@galacticrockets9522]

Looks Great Cant wait to see how far this goes.

[@Tevorieriest]

That geyser shot

[@SuS_NuG_It]

This was actually remarkably not as funny as I was expecting. And it wasn't even cause of frog man, this game just doesn't look fun. It doesn't seem like it has a lot in it.

[@Jasmin.amoule]

What is a pump fuel Injector ?

[@Daddy_Damo]

Awesome! Cant wait to see how it goes

[@manuraju2288]

Liked it how much did it cost

[@tormachinc]

Great work!

[@tristanlongangue5671]

Why not making it round?

[@jyotiradityabhardwaj4018]

what is a pressure transducer

[@chadjensenster]

Measures pressure and outputs a 4-20 mA signal that can be read by a computer