Max take off weight.
Fighter jet fuel tank capacity.
Perhaps about 590 miles based on.
Aerial refueling also referred to as air refueling in flight refueling ifr air to air refueling aar and tanking is the process of transferring aviation fuel from one military aircraft the tanker to another the receiver during flight.
The cockpit and its bubble canopy give the pilot unobstructed forward and upward vision and greatly improved vision over the side and to the rear.
Thrust 2 x 7 5 t limit load factors 3 2 g 9 g.
145 503 kg 320 776 lbs max landing weight.
Fuel external up to 6 7 t 14 700 lbs external load 9 5 t 21 000 lbs store stations.
8 051 kg 17 749 lbs fuel tank capacity.
1 520 mph mach 2 3 at 50 000 ft maximum fuel capacity.
About 60 000 lb hr at mach 2 3 at 50 000 ft for the f 15a with.
370 imp gal of extra fuel per fighter that p 38s could carry out operation vengeance the downing of admiral isoroku yamamoto s airplane.
Saab gripen e engine gripen e fighter jet is powered by general electric ge f414g turbofan engine with 22 000 lb 98 kn of.
With a full load of internal fuel the f 16 can withstand up to nine g s nine times the force of gravity which exceeds the capability of other current fighter aircraft.
For this mission each fighter carried one drop tank of approximately 150 to 165 us gal 570 to 620 l and a larger one of approximately 300 to 330 us gal 1 100 to 1 200 l.
The two main refueling systems are probe and drogue which is simpler to adapt to existing aircraft and the flying boom which offers faster fuel.
3 475 gal 23 280 lb internally with conformal fuel tanks fuel flow rate.
Total 14 heavy wet 5 performances max.
The aircraft s internal fuel tank with a combined capacity of 3 4 tons is about 40 larger than the previous version.
The increase in volume is made possible by moving the landing gear from the fuselage to the inner wing.