Thrust to Power Ratios for Modern Propulsion Systems

AI Thread Summary
Thrust to power ratios for modern propulsion systems vary significantly based on vehicle type and speed. A reference cited indicates a thrust to power ratio of 0.016 N/W for a DC-9 jet engine, but the accuracy of this figure is questioned. The discussion highlights that these ratios can be more meaningful when considering efficiency curves rather than fixed numbers. Participants express uncertainty about where to find comprehensive data on thrust to power ratios across different propulsion systems. Overall, the conversation emphasizes the complexity and variability of these ratios in practical applications.
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Does anybody know some ballpark figures for thrust to power, Newtons per watt, ratios for modern propulsion systems, mechanical drive train ie cars trucks, propeller driven craft, boats planes, and rockets.

I've found one reference that states the F/P ratio for a DC-9 jet engine is 0.016 N / W. Is that accrurate?

Thanks,

Fred
 
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I'm not sure such a ratio has any meaning, since for most vehicles it varies with speed.
 
Yes, I've read that efficiency numbers for propeller driven air craft very with the vehicles air speed.

Curves would do just as well.

I just am clueless as to where to start looking for that information.
 
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