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  2. Escape velocity - Wikipedia

    en.wikipedia.org/wiki/Escape_velocity

    Escape speed at a distance d from the center of a spherically symmetric primary body (such as a star or a planet) with mass M is given by the formula [2] [3] = = where: G is the universal gravitational constant (G ≈ 6.67 × 10 −11 m 3 ⋅kg −1 ⋅s −2 ‍ [4])

  3. Characteristic energy - Wikipedia

    en.wikipedia.org/wiki/Characteristic_energy

    After reducing the problem to the relative motion of the bodies in the plane, he defines the constant of the motion c 3 by the equation2 + ẏ 2 = 2k 2 M/r + c 3, where M is the total mass of the two bodies and k 2 is Moulton's notation for the gravitational constant. He defines c 1, c 2, and c 4 to be other constants of the

  4. Two-body problem - Wikipedia

    en.wikipedia.org/wiki/Two-body_problem

    The resulting equation: ¨ = shows that the velocity = of the center of mass is constant, from which follows that the total momentum m 1 v 1 + m 2 v 2 is also constant (conservation of momentum). Hence, the position R ( t ) of the center of mass can be determined at all times from the initial positions and velocities.

  5. 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

  6. Specific orbital energy - Wikipedia

    en.wikipedia.org/wiki/Specific_orbital_energy

    Thus the hyperbolic excess velocity (the theoretical orbital velocity at infinity) is given by = / However, Voyager 1 does not have enough velocity to leave the Milky Way. The computed speed applies far away from the Sun, but at such a position that the potential energy with respect to the Milky Way as a whole has changed negligibly, and only ...

  7. Tsiolkovsky rocket equation - Wikipedia

    en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation

    A rocket's required mass ratio as a function of effective exhaust velocity ratio. The classical rocket equation, or ideal rocket equation is a mathematical equation that describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity and can thereby move due to the ...

  8. Schwarzschild radius - Wikipedia

    en.wikipedia.org/wiki/Schwarzschild_radius

    This expression had previously been calculated, using Newtonian mechanics, as the radius of a spherically symmetric body at which the escape velocity was equal to the speed of light. It had been identified in the 18th century by John Michell [ 6 ] and Pierre-Simon Laplace .

  9. Ergosphere - Wikipedia

    en.wikipedia.org/wiki/Ergosphere

    2 Radial pull. 3 Ergosphere size. 4 References. ... it is still possible for objects that enter that region with sufficient velocity to escape from the gravitational ...