Talk:Microturbo TRI 60

External links modified (January 2018)
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Specifications - thrust specific fuel consumption.
A slight headache here.

The article stated: 1.1 kg/(daN h) (1.03 lb/(lbf h)).

But that is by definition incorrect because:


 * 1.1 kg/(daN⋅h) works out as 30.56 g/(kN s), which converts to 1.079 lb/(lbf⋅h)


 * 1.03 lb/(lbf⋅h) converts to 29 g/(kN⋅s)

Given the French origin of this design, I'll assume 1.1 kg/(daN⋅h) is from the source. The convert template doesn't know about kg/(daN⋅h). So I'll go with 30.6 g/(kN⋅s) - it's 30.56 g/(kN⋅s) to 4SF.

This could very well be very wrong.

Michael F 1967 (talk) 02:27, 2 September 2019 (UTC)