This appeared up on the Air Power Australia media page earlier today.
http://www.ausairpower.net/APA-NOTAM-160407-1.html
Have checked the figures and can't fault them. Can anyone else?
FYI, based on some of the configurations/weapons loads that are around in various briefings and papers, the F-22 would likely have a higher MIFW. Given the structural layout and extensive use of titanium this is highly probable.
Enjoy.
For rjmaz1: check out F-22 fuel load, empty weight and then you might want to learn a bit about SFC and how performance testing is really done. Hint - Certainly not on the basis of fuel fraction proportionality.
http://www.ausairpower.net/APA-NOTAM-160407-1.html
Have checked the figures and can't fault them. Can anyone else?
FYI, based on some of the configurations/weapons loads that are around in various briefings and papers, the F-22 would likely have a higher MIFW. Given the structural layout and extensive use of titanium this is highly probable.
Enjoy.
For rjmaz1: check out F-22 fuel load, empty weight and then you might want to learn a bit about SFC and how performance testing is really done. Hint - Certainly not on the basis of fuel fraction proportionality.
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