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Aircraft Mechanics
Weight of Aircraft at End of Cruise Phase in Aircraft Design Formulas
Weight of Aircraft at End of Cruise Phase is the weight before the loitering/descent/action phase of the mission plan. And is denoted by W
f
. Weight of Aircraft at End of Cruise Phase is usually measured using the Kilogram for Weight. Note that the value of Weight of Aircraft at End of Cruise Phase is always positive.
Aircraft Design formulas that make use of Weight of Aircraft at End of Cruise Phase
f
x
Optimum Range for Jet Aircraft in Cruising Phase
Go
f
x
Optimum Range for Prop-Driven Aircraft in Cruising Phase
Go
f
x
Velocity for Maximizing Range given Range for Jet Aircraft
Go
f
x
Preliminary Endurance for Jet Aircraft
Go
FAQ
What is the Weight of Aircraft at End of Cruise Phase?
Weight of Aircraft at End of Cruise Phase is the weight before the loitering/descent/action phase of the mission plan. Weight of Aircraft at End of Cruise Phase is usually measured using the Kilogram for Weight. Note that the value of Weight of Aircraft at End of Cruise Phase is always positive.
Can the Weight of Aircraft at End of Cruise Phase be negative?
No, the Weight of Aircraft at End of Cruise Phase, measured in Weight cannot be negative.
What unit is used to measure Weight of Aircraft at End of Cruise Phase?
Weight of Aircraft at End of Cruise Phase is usually measured using the Kilogram[kg] for Weight. Gram[kg], Milligram[kg], Ton (Metric)[kg] are the few other units in which Weight of Aircraft at End of Cruise Phase can be measured.
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