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  2. Velocity, Inc. - Wikipedia

    en.wikipedia.org/wiki/Velocity,_Inc.

    Velocity, Inc. is an American kit aircraft manufacturer. The company was founded in 1984 by Danny Maher, marketing a four-seat homebuilt aircraft based on the Long-EZ design. The first prototype flew in 1985. The company was sold to Scott and Duane Swing in 1992. In 1995, the cockpit design was changed, adding a gull wing door design. [1]

  3. Velocity XL - Wikipedia

    en.wikipedia.org/wiki/Velocity_XL

    The Velocity XL (XL: Extra Large) is an American amateur-built aircraft, produced by Velocity, Inc. It is an enlarged version of their Velocity SE canard pusher design. [ 1 ] [ 2 ]

  4. Velocity SE - Wikipedia

    en.wikipedia.org/wiki/Velocity_SE

    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.

  5. Velocity V-Twin - Wikipedia

    en.wikipedia.org/wiki/Velocity_V-Twin

    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 ...

  6. V speeds - Wikipedia

    en.wikipedia.org/wiki/V_speeds

    The minimum speed that the aircraft is still controllable with the critical engine inoperative [21] while the aircraft is airborne. V MCA is sometimes simply referred to as V MC. V MCG: Minimum control speed ground. The minimum speed that the aircraft is still controllable with the critical engine inoperative [21] while the aircraft is on the ...

  7. Flight envelope - Wikipedia

    en.wikipedia.org/wiki/Flight_envelope

    A chart of velocity versus load factor (or V-n diagram) is another way of showing limits of aircraft performance. It shows how much load factor can be safely achieved at different airspeeds. [3] At higher temperatures, air is less dense and planes must fly faster to generate the same amount of lift.