@DESERT FIGHTER
^^^specs plz...:)
Or better if u could provide me a link as very little info is available online. Plus it won't divert the topic...:agree:
@Abu Zolfiqar
Let me rephrase the my question, i mean what kind of engine does Huma use n any performance specifications n is Pak Army satisfied with its performance?:)
Can u plz provide a link for that, just for clarification nothing else...:)
Btw what i was saying is that RD180 is a closed loop engine n here is what wiki says :
Sorry i didn't knew RD180 is a Semi cryogenic engine, plz pardon my ignorance, told ya i not an expert in these matter...:)
@S-DUCT
AFAIK RL-10 is not closed loop engine although NASA uses it for the Centaur stage but the first stage is still powered by RD180 in Atlas V.
I m no expert so plz feel free to point out my mistakes....:)
Very true thats why the Americans r still using RD180 for their Atlas V, i guess.
The European engine ur talking about is the French
Vinci (rocket engine) which is still undervelopment....:)
@S-DUCT
Does ISRO plan to use only Semi Cryogenic engine for 2nd stage in future or it will be upgraded to cryogenic engine in future as in Araine 5.
Btw what r ur thoughts about development of a closed loop cryogenic engine by ISRO n its future prospects???:)
N @S-DUCT will SC160 will...
@SpArK @S-DUCT @gslv mk3 @sancho @IND151
Can u guys provide some info on the Semi Cryogenic 2000kn SC160 engine being developed by ISRO to replace L110...:undecided:
Has its development completed or not? N will it be used in the April 2014 launch or not?
Plus any other info...