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- #21
Wmaxt, if I am understanding you correctly, you are saying that the Mustang's original 1,720hp is down to just 1,400hp by 30-32,000ft. I think that sounds too optimistic.
I wish we had a hp / altitude chart. You would think that they would be floating around by the dozens.
Robert Goebel flew Mustangs with the 31st Fighter Group, based at San Severo, Italy, in the MTO (Mediterranean Theater of Operations).
The P-51 had a two-stage blower in the induction system that was controlled automatically with a barometric switch. Around 17,000 feet, when the throttle had been advanced almost all the way forward just to maintain normal cruise, the blower would kick into high, the manifold pressure would jump up, and the climb could be continued to 30,000 feet. The P-51 could be taken a lot higher than that, but above 30,000 feet the power was way down and the controls had to be handled gingerly.
From: http://home.att.net/~jbaugher1/p51_13.html
The P-51H could develop 2,218hp at WEP at 10,200ft. By 20,000ft, it was already down to 1,900hp.
I wish we had a hp / altitude chart. You would think that they would be floating around by the dozens.
Robert Goebel flew Mustangs with the 31st Fighter Group, based at San Severo, Italy, in the MTO (Mediterranean Theater of Operations).
The P-51 had a two-stage blower in the induction system that was controlled automatically with a barometric switch. Around 17,000 feet, when the throttle had been advanced almost all the way forward just to maintain normal cruise, the blower would kick into high, the manifold pressure would jump up, and the climb could be continued to 30,000 feet. The P-51 could be taken a lot higher than that, but above 30,000 feet the power was way down and the controls had to be handled gingerly.
From: http://home.att.net/~jbaugher1/p51_13.html
The P-51H could develop 2,218hp at WEP at 10,200ft. By 20,000ft, it was already down to 1,900hp.