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The Gulfstream G650 is a large business jet produced by Gulfstream Aerospace. [3] The model is designated Gulfstream GVI in its type certificate. [4] The aircraft can be configured to carry from 11 to 18 passengers over a range of 7,000 nautical miles [nmi] (13,000 km; 8,100 mi) at a top speed of Mach 0.925 (530.6 kn; 982.7 km/h; 610.6 mph).
The range is 500 nautical miles longer than the jet's predecessor — the Gulfstream G650. The range and speed helped Gulfstream break a world record for the fastest "round-the-world" flight in 2019.
In November 2011, the Gulfstream G650 received its provisional type certificate (PTC) from the FAA. This cleared the way for the company to begin interior completions of the ultra-large-cabin, ultra-long-range business jet in preparation for customer deliveries in the second quarter of 2012, as originally planned.
The wing is a supercritical design with a 0.87 to 0.88 drag divergence Mach number depending upon lift coefficient. [41] It is based on the G650's wing design with the same 36° sweep. The G600's wingspan will be 8 ft (2.4 m) wider than the G500, allowing for 11,250 lb (5,100 kg) [12] of additional fuel. Both models have a new tail design based ...
A Gulfstream G650 private jet (not Jordan's) pictured in flight. Urbanandsport/NurPhoto via Getty Images It has a maximum range of 8,630 miles, which is enough to reach Tokyo from Florida.
Gulfstream and the Parker Aerospace Control Systems Division have been working together since the program's launch to design and certify the G650's fully digital, fly-by-wire flight control system ...
It is then ferried to Dallas, Texas, for interior finishing and painting. [2] [11] [13] Its wing is a new design, using the Gulfstream G550 airfoil, and has a larger area of 495 ft 2 vs. 369 ft 2 of the G200. This allows the business jet to climb directly to 43,000 ft (13,000 m).
The Gulfstream II is a twin-jet swept wing corporate transport powered by two Rolls-Royce Spey turbofan engines and designed to provide high speed and long range capability without sacrificing the airport performance, reliability, and other operational advantages of its predecessor, the turboprop Gulfstream I. Preliminary design of the wing was ...