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5 dni temu · This page shows a schematic drawing of a pitot-static tube. Pitot-Static tubes, which are also called Prandtl tubes, are used on aircraft as speedometers. The actual tube on the aircraft is around 10 inches (25 centimeters) long with a 1/2-inch (1 centimeter) diameter.
4 dni temu · IRS Options Sub-Menu: Under the SIMULATION menu (page 1), an IRS OPTIONS sub-menu at LSK 6R contains options related to the aircraft’s Inertial Reference Systems. ALIGNMENT TIME: Normally, the IRS takes approximately ten minutes to align, during which the aircraft cannot be moved.
5 dni temu · The Archer LX is powered by a 180-horsepower Lycoming IQ-360-B4A engine and has a cruising speed of 128 knots. The propeller has two blades and is made by Sensenich. The aircraft is equipped with the Garmin G1000 NXi avionics suite, which is a glass cockpit system that provides pilots with a wide range of information on electronic displays.
5 dni temu · Maximum Flight Time The thrust, specific fuel consumption, and fuel load determine the maximum flight time available to the aircraft. \(\LARGE t_{\text{max}} = \frac{M}{TSFC \cdot F} \)
4 dni temu · The Dassault Mirage 2000 is a French multirole, single-engine, delta wing, fourth-generation jet fighter manufactured by Dassault Aviation.It was designed in the late 1970s as a lightweight fighter to replace the Mirage III for the French Air Force (Armée de l'air).The Mirage 2000 evolved into a multirole aircraft with several variants developed, with sales to a number of nations.
4 dni temu · NASA operates two ER-2 aircraft as readily deployable high altitude sensor platforms to collect remote sensing and in situ data on earth resources, atmospheric chemistry and dynamics, and oceanic processes. The aircraft also are used for electronic sensor research and development, satellite calibration and satellite data validation.
5 dni temu · Online flight computer : it enables you to calculate many thins such as true altitude, density alitude, ground speed, true air speed, Mach number, flight time, fuel consumption, units conversion, temperature ride, point of safe return, triangle of velocities, wind components, etc.
