pakistanipower don't really know what is
difference, between Dry Thrust (w/o afterburner), and Wet thrust (w. afterburner).
- Empty weight: 18,900 lb (8,570 kg)
- Internal fuel: 7,000 pounds (3,200 kg)
Thrust/weight: 1.095 (1.24 with loaded weight & 50% internal fuel)
So, from the above, the empty weight of F-16,
plus, 50% internal fuel is:
8,570 kg + (3,200kg * 0.50) =
10,170kg
The Dry Thrust (w/o afterburner) = 76.3 kN or
7,780kg
Wet Thrust (w. afterburner) = 127 kN =
12,950kg
Wet Thrust > Flying Weight > Dry Thrust
12,950kg > 10,170kg > 7,780kg
Dry Thrust to Weight Ratio =
0.765
Wet thrust to Weight Ratio =
1.27
So, we can see, the TWR, w/o AB =
0.765, which is less than 1.0. That means
the F-16 can not lift itself vertically, without the use of AB.
And Wet thrust to Weight Ratio = 1.27,
so it must turn the AB on, if the pilot wants to do a vertically climb, when carrying 50% internal fuel.
The shock diamond is only visible, when the AB is turned on
full blast, not when its only just turned on moderately, which you see only the flaming red butt.
@pakistanipower said he has an engineering background. I wonder what engineering school, he went to. He doesn't seem to have an education, beyond the elementary school.
Otherwise, he would not have failed to do such elementary calculations.