Originally posted by MiG
This is a pretty dodgy calc with assumptions and dodgy info, but it's about 50 MW at full thrust (not cruising thrust) at 35,000 feet and 900 km/h (I assumed the speed because I cbf working out what Mach 0.85 at 35,000 feet is.)
This is using thrust data at high altitude for a RB211, but I don't know which version. I know that Qantas 747s use the RB211-524G.
This is a pretty dodgy calc with assumptions and dodgy info, but it's about 50 MW at full thrust (not cruising thrust) at 35,000 feet and 900 km/h (I assumed the speed because I cbf working out what Mach 0.85 at 35,000 feet is.)
This is using thrust data at high altitude for a RB211, but I don't know which version. I know that Qantas 747s use the RB211-524G.


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