How much fuel does a g4 hold?
G450: The total usable capacity of fuel tanks is 29,500 pounds, or 4,370 U.S. gallons at a standard fuel weight of 6.75 pounds per gallon. The international equivalent is 13,380 kilograms or 16,542 liters.
What is the range of a Gulfstream g4?
Gulfstream G IV Specs
| Performance | |
|---|---|
| Range | 3,800 nm |
| Range | 6,115 km |
How much fuel does a giv hold?
Maximum takeoff and landing weights are increased by 15%. It has a new semi supercritical wing for a fuel capacity of 41,000–12,000 lb (18.6–5.4 t) more than the G-IV.
How much does a Gulfstream GIV-SP cost?
Acquisition cost for the Gulfstream GIV-SP typically ranges from $6-$8 million, on the higher end of its competition such as the Global XRS and Falcon 900 (twice the price of this aircraft).
How much jet fuel does a private jet use?
So, in conclusion, private jets will burn anywhere from 50 gallons of fuel per hour, all the way up to 626 gallons per hour. Of course, keep in mind that these figures are based on the average fuel consumption. Therefore, if you were to look at the burn during take-off and climbing, these figures would be much larger.
How much fuel does a Gulfstream G650 burn per hour?
Gulfstream G650 Gulfstream’s G650 burns right around 452.70 gallons of fuel per hour. At $5.00 a gallon, fuel is going to cost you $2,263.50 per hour.
How many hours can a G4 fly?
So if you can fly direct, can you fly nonstop?
| Aircraft Type | Maximum Range | Maximum Flight Time |
|---|---|---|
| Turboprop | 1000-1500 miles | 4-5 hours |
| Light Jet | 1000-1800 miles | 5 hours |
| Midsize Jet | 2000-3000 miles | 6 hours |
| Supermid Jet | 3000-4000 miles | 7 hours |
How fast does a G4 fly?
It has a maximum speed of 935 km/h (Mach 0.88 (505 knots, 581 mph) and has a cruise speed of 850 km/h (Mach 0.80 (460 knots, 528 mph).
How fast does a Gulfstream 4 go?
It has a maximum speed of 935 km/h (Mach 0.88 (505 knots, 581 mph) and has a cruise speed of 850 km/h (Mach 0.80 (460 knots, 528 mph). It has a length of 26.9 m (88 ft 4 in) and an overall height of 7.44 m (24 ft 5 in) which makes room for a crew of 2 pilots and up to 16 passengers.
What is the range of a giv?
Specifications
| GIV | G350 | |
|---|---|---|
| Range | 4,220 nmi (7,815 km) | 3,800 nmi (7,038 km) |
| Service ceiling | 45,000 ft (13,716 m) | |
| Engines (×2) | Rolls-Royce Tay 611-8 | Rolls-Royce Tay 611-8C |
| Thrust | 13,850lbf / 61.6kN |
How much is a Gulfstream 4?
The G400 had grown out of the Gulfstream IV (GIV), which first entered service in 1987 and set several world records in its class. A new Gulfstream G450 will currently cost between $38m to $43m. A pre-owned model will typically cost anywhere in the $14m to $35m range….The Costs to Own and Operate a Gulfstream G450.
| Item | Costs |
|---|---|
| Total Variable Cost per Hour | $3,822 |
How much does 1 gallon of jet fuel cost?
170.8 Cents (US dollars) per Gallon.
What are the specs of a Gulfstream IV?
It has a take off distance of 1,609 meters and a landing distance of 1,521 meters. The aircraft has a rate of climb of 4,219 feet per minute. The Gulfstream IV is capable of carrying a maximum payload of 1,542 kg and has a fuel tank capacity of 3513.6 US Gal. The maximum take off and landing weight are 33,203 kg and 26,535 kg respectively.
Is the Gulfstream IV a twin engine aircraft?
The Gulfstream IV is a twin engine jet aircraft designed and produced by Gulfstream Aerospace from 1985 to 2018. Developed as a re-engined, extended fuselage of Gulfstream III, this aircraft that provides a higher maximum take off weight, delivers lower noise, and a better fuel efficiency.
What’s the difference between a Gulfstream IV and G450?
G350/G450. The G450 is a designation for the model GIV-X, approved by the FAA on August 12, 2004, as is the G350, which has a reduced fuel capacity. Compared to the Gulfstream IV, its fuselage is 12 inches longer and the main entry door relocated aft.
What are the benefits of Gulfstream IV wing?
The Gulfstream IV wing has a weaker, more swept outboard shock resulting in a lower cruise drag. Other benefits arising from this design are a lower root bending moment due to the more inboard center of pressure, a lower stall speed due to washout and a larger fuel volume due to increased chord.