1 520 mph mach 2 3 at 50 000 ft maximum fuel capacity.
Fighter jet fuel tank capacity.
3 475 gal 23 280 lb internally with conformal fuel tanks fuel flow rate.
It was only with drop tanks supplying 450 us gallons 1 700 l.
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.
Thrust 2 x 7 5 t limit load factors 3 2 g 9 g.
Aircraft fuel tanks are a major component of aircraft fuel systems they can be classified into internal or external fuel tanks and can be further classified by method of construction or intended use.
Max take off weight.
Total 14 heavy wet 5 performances max.
About 60 000 lb hr at mach 2 3 at 50 000 ft for the f 15a with.
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.
8 051 kg 17 749 lbs fuel tank capacity.
145 503 kg 320 776 lbs max landing weight.
The increase in volume is made possible by moving the landing gear from the fuselage to the inner wing.
The aircraft s internal fuel tank with a combined capacity of 3 4 tons is about 40 larger than the previous version.
Saab gripen e engine gripen e fighter jet is powered by general electric ge f414g turbofan engine with 22 000 lb 98 kn of.
Perhaps about 590 miles based on.
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.
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.
Safety aspects of aircraft fuel tanks were examined during the investigation of the 1996 twa flight 800 in flight explosion accident.