4throck
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Ok, this is n00b question but I'm confused with the MainThrust and ISP values used on the SC3 Atlantis.
On the config we have:
Main_Thrust=53400
ISP=5000
But on Astronautix, Wikipedia, etc, the values are:
Main Thrust = 1859 kN
ISP = 453s
Effective exhaust velocity = 4440 m/s
[ame="http://en.wikipedia.org/wiki/Space_Shuttle_Main_Engine"]http://en.wikipedia.org/wiki/Space_Shuttle_Main_Engine[/ame]
I understand that Orbiter ISP will be s*9.8066, (or exhaust) so ISP=5000 is approximate.
But for thrust I don't understand. It should be Main_Thrust = 1859000*3 = 5577000.
And in this case shouldn't ISP be tripled?
Sorry for such a basic question, but I've searched the Forum, the SC3 and Orbiter docs, etc and didn't find an answer with any real world examples. :facepalm:
On the config we have:
Main_Thrust=53400
ISP=5000
But on Astronautix, Wikipedia, etc, the values are:
Main Thrust = 1859 kN
ISP = 453s
Effective exhaust velocity = 4440 m/s
[ame="http://en.wikipedia.org/wiki/Space_Shuttle_Main_Engine"]http://en.wikipedia.org/wiki/Space_Shuttle_Main_Engine[/ame]
I understand that Orbiter ISP will be s*9.8066, (or exhaust) so ISP=5000 is approximate.
But for thrust I don't understand. It should be Main_Thrust = 1859000*3 = 5577000.
And in this case shouldn't ISP be tripled?
Sorry for such a basic question, but I've searched the Forum, the SC3 and Orbiter docs, etc and didn't find an answer with any real world examples. :facepalm: