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aerospace defense system مؤسسة لتطوير انظمة الدفع انشئت بهندسة الطيران والفضاء
this is not a waste of time falcon 9 / control-ability test.
altitude :250 m ,latitude :100m
A mature solid rocket blasts in to 33 km / on board cams.
Ares I solid rocket booster static test / 22 million HP
vacuum engine firing /zero back pressure
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...
13/11/2012
وقود جديد تطوره المجموعة يعمل في درجة حرارة 2 سلزيوس 200 جم تنتج 20 بار في حجم ا لتر
09/11/2012
ابتكار قام به كل من احمد سمير واحمد ابراهيم كلية الهندسة قسم هندسة الطيران والفضاء يقوم بحرق غاز البروبان ويولد قوة دفع رائعة تستخدم لتسيير المركبات
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Cairo Univeristy
Giza
12511