MARS

Engine type : liquid propellant rocket engine.
test : static test.
Max thrust : 6.5 ton .
burning time : 20 sec.
fuel type : liquid alcohol.
oxidizer : liquid oxygen.
Propellant : 14 kg liquid alcohol+18 kg of liquid oxygen.
propellant tank : 2 tanks each 350 litres.
engine coolant : liquid nitrogen.
tank material :alcohol tank of steel ,oxygen tank of aluminum.
test pad coolant system :pressurized water 27 bar.
test pad coolant feed :125 litre/sec.
test secured area :200 m away from test pad.
count down start :T-10 minutes................................................................................................

https://www.youtube.com/watch?v=i1pRXKewNfM

TM65 Episode 2 - Static Test af a 65KN Liquid propellant rocket engine. In English: This video shows the preparations and the test launch of one of the world's largest amateur-built liquid rocket engines. We present a unique insi...

وقود جديد تطوره المجموعة يعمل في درجة حرارة 2 سلزيوس 200 جم تنتج 20 بار في حجم ا لتر