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gf0012-aust;183718]There is an obvious issue with using that metric in isolation. the fundamental issue on through life support is the maint and robustness of the components. if the engine has 1/3rd the availability rate of an F404 (for example), then the amount of time in the air relative to fuel is still subjected to wear and tear
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I believe your post support just what they state.
If one look at the capability and mission of choice, there are very few aircraft that can perform longer intercept mission with out having to land to refuel or an mid-flight refuel.
Those UB clearly have that capability.
But i wonder who would pay up for mission like this..?
Its gonna cost lots of buck anyway..
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metrics are quite diverse and varied - its why we take so long in determining TLS for aircraft (or for any platform for that matter)
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Well metrics works, it's just what one choose to put in the equation.
And which requirements put up.
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that metric could not be a baseline condition because it can not ignore the basic TLS and sustainment issues.
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Its not that hard to calculate the metric of those UB, remeber they are not gonna perform under any airforce regulation and doctrine.
Hense they can skip many variables.
Thanks