Above 100,000 feet altitude (20 miles).
It is 87 km of altitude.
The higher the altitude the lower the temperature.
Altitude describes an object's position relative to sea level. An object in a position higher than sea level would have a positive altitude, sea level would have an altitude of zero, and any object below sea level would have a negative altitude.
There are many things that could happen as the altitude of the sun increases. As altitude increases the temperature usually does too.
Service Ceiling: 43,100ft (13,140m)
Depends on the cruise altitude, & the weather at the time. Typically around -40degrees Celsius, at FL 33,000 ft.
The Boeing 777 can fly up to altitudes of 43,100ft, however, its normal cruising attitude is anywhere between 35,000 feet and 39,000 feet.
The stall speed of an aircraft depends on its altitude, weight, configuration, and lateral and vertical acceleration. The stall speed for a 777 is dependent on these real-time factors.
Around 40,000 feet depending on wind and gross weight
Both, the Boeing 777 and the Boeing 787 have extremely long range than any other airplanes. The Boeing 777 is very old and it been around much longer than the Boeing 787. The Boeing 777 can also carry more passengers than the Boeing 787 but the Boeing 787 is lighter, can take off faster and easier, can travel faster and has more longer range than the Boeing 777. The Boeing 777 is heavier than the Boeing 787. Size does not even matter but the altitude and the range! Top speed of the Boeing 777: 567 miles per hour Top speed of the Boeing 787: 677 miles per hour Maximum cruising altitude of the Boeing 777: 43, 400 ft Maximum cruising altitude of the Boeing 787: 45, 200 ft
A Boeing 777 has a maximum cruise speed of 0.89 Mach (590 mph, 950 km/h, 512 knots) at 35,000 ft (11,000 m) cruise altitude.
The vertical distance of the aircraft above the surface.
Their proportion remains almost the same with altitude however the absolute number falls off as the pressure decreases with altitude.
There are two types of maximum altitude. The first is set by the FAA and is known as Service Ceiling and the second is the maximum altitude, above sea level, at which an aircraft can maintain horizontal flight under standard atmospheric conditions. This is called Absolute Ceiling. Absolute ceiling is also affected by another factor: weight.
An absolute ceiling is the maximum altitude above sea level at which an aircraft or missile can maintain horizontal flight under normal conditions.
0.89 Mach (590 mph, 950 km/h, 512 knots) at 35,000 ft (11,000 m) cruise altitude