The localhost fm commands page can be used to get total aircraft weight for a certain fuel percentage. The way of getting it is kind of convoluted because the fuel percent commands are based on with drop tanks…so you have to figure out what percentage of total fuel is 50% internal fuel etc.
The way to short cut this is to just load in with 50% internal on fuel slider…look at the time…and then adjust the percentage in localhost command until it matches the 50% internal time.
I know, I was just saying that in local host proper you can’t see the total mass (as feet explained you can only see it though fm commands), but can still see your fuel mass, since @Godvana was talking about localhost proper
Cool charts. A representation of already known values but better than ‘max-pull’, assuming wing coeff is in direct relation to SEP it paints a clearer picture. Doesn’t provide any insight on where the Gripen should be though.
Question is what is it’s relation to the already correct STR (aside from the 1.3-1.7°/0.5-0.7° pointed out by Gio/devs), and what is it’s relation to SEP… Or is this disparity just a result of instability not being modelled
i think this is their way of trying to emulate the lower AoA needed for specific lift at a specific radius.
And they have probably in the process miscalculated somewhere.
TLDR:
when it turns it does not loose speed as fast as it should, some argue it should be at the same level as F-16 or M2K. personally i think it should be at about 30% better. before todays change it was 100% better, no clue about the current numbers.
Mirage 2000 has good low efficiency and then experiences massive drag penalty near its AoA limit. If you do max performance turn in Mirage 2000 you will lose speed at high rate.
New changes to Gripen do not alter drag factor in any noticeable way.
180% last I checked, and it’s not feasible to say the Gripen should have 30% improved specific excess power over the F-16 when the aspect ratio is superior, thrust to weight significantly higher on the F-16.