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The absolute ceiling and service ceiling diagram of an aircraft. With respect to aircraft performance, a ceiling is the maximum density altitude an aircraft can reach under a set of conditions, as determined by its flight envelope.
|endurance= – the maximum flight endurance of the aircraft, where the range is unknown (this is particularly common in specifications of early aircraft). |ceiling= – the service ceiling of the aircraft |glide ratio= – the maximum glide ratio of an aircraft. Please only include this specification when describing gliders and sailplanes.
Coffin corner (also known as the aerodynamic ceiling [1] or Q corner) is the region of flight where a fast but subsonic fixed-wing aircraft's stall speed is near the critical Mach number, at a given gross weight and G-force loading. In this region of flight, it is very difficult to keep an airplane in stable flight.
Imperial units templates. Use for US and UK aircraft ... Dimensions Length: ft in: m ... Service ceiling: ft: m Rate of climb:
The outer edges of the diagram, the envelope, show the possible conditions that the aircraft can reach in straight and level flight. For instance, the aircraft described by the black altitude envelope on the right can fly at altitudes up to about 52,000 feet (16,000 m), at which point the thinner air means it can no longer climb.
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A sectional chart is a two-sided chart created from a Lambert Conformal Conic Projection [1] with two defined standard parallels. The scale is 1:500,000, with a contour interval of 500 feet. The size of each sectional is designed to be "arm's width" when completely unfolded.
Aircraft name goes here Image caption: Description Role: Crew: First Flight: Entered Service: Manufacturer: Dimensions Length: m: ft in Wingspan: m: ft in Height: m ...