Commercial Airlines normally retract the landing gear when the Vertical Speed Indicator indicates a positive rate of climb. Basically, when the instruments indicate the sircraft is climbing, the gear is raised.
Cruising altitude is an economical height for an aircraft to fly. It is also a choice made in view of other aircraft routes.
DA-Decision Altitude. It is the lowest an aircraft can fly on an (precision) instrument approach. At that height the pilot must be able to see the runway or landing light system or else he has to initiate a missed approach
If you grossly overcharged the struts of the landing gear you could increase the ride height of the aircraft, but it could lead to damage to the aircraft due to the lack of 'give' when landing and it would be very uncomfortable for those on board. It would not therefore be sensible.
Yes, it is called an altimeter. There are two types: pressure and radar. Pressure altimeters use barometric pressure to calculate height above sea level or MSL. Radar Altimeters use Radio signals to calculate height above ground level. They are usually only used during approach to landing and are rarely found on lighter aircraft.
The altitude at which an aircraft is travelling does affect its speed because the thinner atmosphere causes less aerodynamic drag.
No, an altitude is a height above sea level.
An odometer is for distance travelled, not height. You need something sensitive to changes in atmospheric pressure, a barometer, for measuring altitude. Altimeters as fitted to aircraft are in effect barometers.
The height is the length of its altitude.
height
The maximum height flown by an aircraft is 37650m(123524ft). The aircraft is Mig-25 Foxbat.
The height or the altitude of the land is its distance above sea level. This is referred to as the elevation of the land.
The higher an aircraft goes the less dense the air is. What this means is there is less air particles surrounding the plane. This has a positive and negative effect on the aircraft. The positive effect is there is less friction on the aircraft allowing for better fuel economy and speeds. The negative effect is that air flow is needed to create lift. If not enough air flows over the wing then not enough lift is produced to keep the aircraft at that height. They counteract this for high altitude aircraft by increasing the speed of the aircraft. It also has an effect on the engines performance. If you get high enough the air becomes so thin that there isn't enough air to support the operations of the engines. this is why there is a mixture lever on many aircraft to allow you to change the fuel/air ration depending on height/