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Why use only pitot-static system for altimeter/airspeed
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10th Feb 2014, 07:26
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Uplinker
Join Date: Nov 1999
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Quote:
engine inlet P2/T2 probes (which have occasionally had icing issues, especially the temp portion) get ~500 watts heat, while aircraft pitot probes get close to a kilowatt at high heat.
Blimey, that's a lot. Didn't realise it was so much.
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