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  2. Celestial mechanics - Wikipedia

    en.wikipedia.org/wiki/Celestial_mechanics

    Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets, satellites, and other spacecraft. The motion of these objects is usually calculated from Newton's laws of motion and the law of universal gravitation .

  3. Orbital mechanics - Wikipedia

    en.wikipedia.org/wiki/Orbital_mechanics

    Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets, satellites, and other spacecraft. The motion of these objects is usually calculated from Newton's laws of motion and the law of universal gravitation .

  4. Category:Celestial mechanics - Wikipedia

    en.wikipedia.org/wiki/Category:Celestial_mechanics

    Download as PDF; Printable version; ... Celestial mechanics is an application of physics, ... Astrodynamics (4 C, 70 P)

  5. Characteristic energy - Wikipedia

    en.wikipedia.org/wiki/Characteristic_energy

    In astrodynamics, the characteristic energy is a measure of the excess specific energy over that required to just barely escape from a massive body. The units are length 2 time −2, i.e. velocity squared, or energy per mass.

  6. Spacecraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_flight_dynamics

    Flight dynamics depends on the disciplines of propulsion, aerodynamics, and astrodynamics (orbital mechanics and celestial mechanics). It cannot be reduced to simply attitude control; real spacecraft do not have steering wheels or tillers like airplanes or ships.

  7. n-body problem - Wikipedia

    en.wikipedia.org/wiki/N-body_problem

    In physics, the n-body problem is the problem of predicting the individual motions of a group of celestial objects interacting with each other gravitationally. [1] Solving this problem has been motivated by the desire to understand the motions of the Sun, Moon, planets, and visible stars.

  8. Orbital inclination - Wikipedia

    en.wikipedia.org/wiki/Orbital_inclination

    In astrodynamics, the inclination can be computed from the orbital momentum vector (or any vector perpendicular to the orbital plane) as = ⁡ | | where is the z-component of . Mutual inclination of two orbits may be calculated from their inclinations to another plane using cosine rule for angles .

  9. Orbital maneuver - Wikipedia

    en.wikipedia.org/wiki/Orbital_maneuver

    In astrodynamics a gravity assist maneuver, gravitational slingshot or swing-by is the use of the relative movement and gravity of a planet or other celestial body to alter the trajectory of a spacecraft, typically in order to save propellant, time, and expense.