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  2. Escape velocity - Wikipedia

    en.wikipedia.org/wiki/Escape_velocity

    An alternative expression for the escape velocity v e particularly useful at the surface on the body is: = where r is the distance between the center of the body and the point at which escape velocity is being calculated and g is the gravitational acceleration at that distance (i.e., the surface gravity). [11]

  3. Orbital mechanics - Wikipedia

    en.wikipedia.org/wiki/Orbital_mechanics

    The formula for an escape velocity is derived as follows. The specific energy (energy per unit mass) of any space vehicle is composed of two components, the specific potential energy and the specific kinetic energy. The specific potential energy associated with a planet of mass M is given by

  4. Characteristic energy - Wikipedia

    en.wikipedia.org/wiki/Characteristic_energy

    But the maximal velocity on the new orbit could be approximated to 33.5 km/s by assuming that it reached practical "infinity" at 3.5 km/s and that such Earth-bound "infinity" also moves with Earth's orbital velocity of about 30 km/s. The InSight mission to Mars launched with a C 3 of 8.19 km 2 /s 2. [5]

  5. Circular orbit - Wikipedia

    en.wikipedia.org/wiki/Circular_orbit

    The formula is dimensionless, describing a ratio true for all units of measure applied uniformly across the formula. If the numerical value a {\displaystyle \mathbf {a} } is measured in meters per second squared, then the numerical values v {\displaystyle v\,} will be in meters per second, r {\displaystyle r\,} in meters, and ω {\displaystyle ...

  6. Parabolic trajectory - Wikipedia

    en.wikipedia.org/wiki/Parabolic_trajectory

    A radial parabolic trajectory is a non-periodic trajectory on a straight line where the relative velocity of the two objects is always the escape velocity. There are two cases: the bodies move away from each other or towards each other. There is a rather simple expression for the position as function of time:

  7. Orbital period - Wikipedia

    en.wikipedia.org/wiki/Orbital_period

    In the special case of perfectly circular orbits, the semimajor axis a is equal to the radius of the orbit, and the orbital velocity is constant and equal to = where: r is the circular orbit's radius in meters, This corresponds to 1 ⁄ √2 times (≈ 0.707 times) the escape velocity.

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  9. Atmospheric escape - Wikipedia

    en.wikipedia.org/wiki/Atmospheric_escape

    One classical thermal escape mechanism is Jeans escape, [1] named after British astronomer Sir James Jeans, who first described this process of atmospheric loss. [2] In a quantity of gas, the average velocity of any one molecule is measured by the gas's temperature, but the velocities of individual molecules change as they collide with one another, gaining and losing kinetic energy.