SYSTEM REQUIREMENTS REVIEW - Purdue University
The Gulfstream G650 currently performs a similar design mission with a fuel consumption rate of 0.158 nm/lbs. This figure was calculated by dividing the maximum range by the maximum fuel weight. The design mission was to reduce current fuel burn by as much as 40%. A reduction of 40% in fuel consumption based upon the G650 would be a fuel burn of .265 nm/lbs. A modern aircraft . that has a ... ................
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