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Gear retraction of a Velocity on takeoff. The Velocity XL is 12 in (310 mm) longer and has a 20 in (510 mm) greater span than the SE. [3] The standard XL has a cruising range of 875 nautical miles (1,620 km; 1,007 mi) and a 75% power cruising speed of 185 knots (213 mph; 343 km/h) air speed.
In March 1997, Velocity introduced the XL model, which features a larger cabin and space for a larger engine. [9] The XL-5, sometimes called a "dash five", was introduced in 2004. It reduced the size of the keel down the center of the cabin, giving more room in the back seat. [10] Velocity has developed a twin-engine model called the Velocity V ...
The Velocity Model 173 SE (Standard Elite) is an entry-level canard pusher aircraft from Velocity Aircraft. [ 1 ] [ 2 ] [ 3 ] The four seat, rear engine aircraft may be powered by a 160 hp (120 kW) Lycoming IO-320 or a 200 hp (150 kW) Lycoming IO-360 engine.
The Velocity V-Twin is a four-seat (with a five-seat option), retractable tricycle landing gear, composite construction aircraft with a twin engine pusher configuration and the canard layout of the Velocity XL single engine aircraft. Its fuselage is that of the XL-RG, with the addition of the single, vertical surface which replaces the twin end ...
The planes were based on the fixed-gear Velocity SE modified by XCOR Aerospace and the retractible gear Velocity XL modified by Armadillo Aerospace for the purpose of rocket racing. The Velocity airframe was derived from a commercially available kit plane that traced its design heritage to the Rutan Long-EZ , which had been modified to accept ...
Originally, it slightly outperformed the .22 LR, but was "not noted for great accuracy", [2] while later smokeless loads achieved about the same muzzle velocity as the .22 LR. [ citation needed ] As with the .22 Winchester Automatic [ 3 ] and .22 Remington Automatic , [ 4 ] the .22 extra long will not chamber correctly in .22 long rifle weapons ...
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V-speed designator Description V 1: The speed beyond which takeoff should no longer be aborted (see § V 1 definitions below). [7] [8] [9]V 2: Takeoff safety speed. The speed at which the aircraft may safely climb with one engine inoperative.