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  2. Terminal velocity - Wikipedia

    en.wikipedia.org/wiki/Terminal_velocity

    Graph of velocity versus time of a skydiver reaching a terminal velocity. Based on air resistance, for example, the terminal speed of a skydiver in a belly-to-earth (i.e., face down) free fall position is about 55 m/s (180 ft/s). [3]

  3. Equations for a falling body - Wikipedia

    en.wikipedia.org/wiki/Equations_for_a_falling_body

    This velocity is the asymptotic limiting value of the acceleration process, because the effective forces on the body balance each other more and more closely as the terminal velocity is approached. In this example, a speed of 50 % of terminal velocity is reached after only about 3 seconds, while it takes 8 seconds to reach 90 %, 15 seconds to ...

  4. Free fall - Wikipedia

    en.wikipedia.org/wiki/Free_fall

    A typical skydiver in a spread-eagle position will reach terminal velocity after about 12 seconds, during which time they will have fallen around 450 m (1,500 ft). [4] Free fall was demonstrated on the Moon by astronaut David Scott on August 2, 1971. He simultaneously released a hammer and a feather from the same height above the Moon's surface.

  5. Speed skydiving - Wikipedia

    en.wikipedia.org/wiki/Speed_skydiving

    The speed, achieved by the human body in free fall, is a function of several factors; including the body's mass, orientation, and skin area and texture. [1] In stable, belly-to-earth position, terminal velocity is about 200 km/h (120 mph). Stable freefall head down position has a terminal speed of 240–290 km/h (around 150–180 mph).

  6. Projectile motion - Wikipedia

    en.wikipedia.org/wiki/Projectile_motion

    The vertical component of the velocity changes linearly, [note 2] because the acceleration due to gravity is constant. The accelerations in the x and y directions can be integrated to solve for the components of velocity at any time t, as follows: = ⁡ (),

  7. Ballistic missile flight phases - Wikipedia

    en.wikipedia.org/wiki/Ballistic_missile_flight...

    The boost phase is the portion of the flight of a ballistic missile or space vehicle during which the booster and sustainer engines operate until it reaches peak velocity. . This phase can take 3 to 4 minutes for a solid rocket (shorter for a liquid-propellant rocket), the altitude at the end of this phase is 150–200 km, and the typical burn-out speed is 7 k

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  9. File:Graph of velocity versus time of a skydiver reaching a ...

    en.wikipedia.org/wiki/File:Graph_of_velocity...

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