isn't that RD93 spec precisely from this link? your F404 SFC source is ...?I have stated the SFC of F404 GE-402. Difference in between 402, RM-12 and IN-20 is the air mass flow and pressure ratio. So you could say that the SFC of all three would be near about same with a little difference.
https://www.uecrus.com/eng/products/military_aviation/rd93/
You could get RD93 specs from this link.
You are stating the SFC of GE in pound opposed to kg in RD93.
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and the F404 wiki
- Specific fuel consumption:
- Military thrust: 0.81 lb/(lbf⋅h) (23 g/(kN⋅s))
- Full afterburner: 1.74 lb/(lbf⋅h) (49 g/(kN⋅s))
49*3600/1000=176.4 kg/kN.hour
how could be?SFC of RD93 with afterburner is 2.05 kg/kgh
SFC of GE F404 with afterburner is 0.78 kg/kgh
SFC of RD93 without afterburner is 0.77 kg/kgh
SFC of GE F404 without afterburner is 0.36 kg/kgh
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