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  2. Momentum exchange tether - Wikipedia

    en.wikipedia.org/wiki/Momentum_exchange_tether

    A momentum exchange tether is a kind of space tether that could theoretically be used as a launch system, or to change spacecraft orbits. Momentum exchange tethers create a controlled force on the end-masses of the system due to the pseudo-force known as centrifugal force. While the tether system rotates, the objects on either end of the tether ...

  3. Barbados - Wikipedia

    en.wikipedia.org/wiki/Barbados

    Barbados ( UK: / bɑːrˈbeɪdɒs / bar-BAY-doss; US: / bɑːrˈbeɪdoʊs / bar-BAY-dohss; locally / bɑːrˈbeɪdəs / bar-BAY-dəss) is an island country in the Lesser Antilles of the West Indies, in the Caribbean region of North America, and is the most easterly of the Caribbean islands.

  4. Angular momentum - Wikipedia

    en.wikipedia.org/wiki/Angular_momentum

    where is the sphere's mass, is the frequency of rotation and is the sphere's radius.. Thus, for example, the orbital angular momentum of the Earth with respect to the Sun is about 2.66 × 10 40 kg⋅m 2 ⋅s −1, while its rotational angular momentum is about 7.05 × 10 33 kg⋅m 2 ⋅s −1.

  5. Hyperbolic trajectory - Wikipedia

    en.wikipedia.org/wiki/Hyperbolic_trajectory

    A radial hyperbolic trajectory is a non-periodic trajectory on a straight line where the relative speed of the two objects always exceeds the escape velocity. There are two cases: the bodies move away from each other or towards each other. This is a hyperbolic orbit with semi-minor axis = 0 and eccentricity = 1.

  6. Orbital state vectors - Wikipedia

    en.wikipedia.org/wiki/Orbital_state_vectors

    Orbital position vector, orbital velocity vector, other orbital elements. In astrodynamics and celestial dynamics, the orbital state vectors (sometimes state vectors) of an orbit are Cartesian vectors of position ( ) and velocity ( ) that together with their time ( epoch) ( ) uniquely determine the trajectory of the orbiting body in space. [1 ...

  7. Orbital maneuver - Wikipedia

    en.wikipedia.org/wiki/Orbital_maneuver

    Orbital inclination change is an orbital maneuver aimed at changing the inclination of an orbiting body's orbit. This maneuver is also known as an orbital plane change as the plane of the orbit is tipped. This maneuver requires a change in the orbital velocity vector ( delta v) at the orbital nodes (i.e. the point where the initial and desired ...

  8. Orbit equation - Wikipedia

    en.wikipedia.org/wiki/Orbit_equation

    In astrodynamics, an orbit equation defines the path of orbiting body around central body relative to , without specifying position as a function of time.Under standard assumptions, a body moving under the influence of a force, directed to a central body, with a magnitude inversely proportional to the square of the distance (such as gravity), has an orbit that is a conic section (i.e. circular ...

  9. Solar Dynamics Observatory - Wikipedia

    en.wikipedia.org/wiki/Solar_Dynamics_Observatory

    Solar Dynamics Observatory. The detailed images recorded by SDO in 2011–2012 have helped scientists uncover new secrets about the Sun. The Solar Dynamics Observatory ( SDO) is a NASA mission which has been observing the Sun since 2010. [4] Launched on 11 February 2010, the observatory is part of the Living With a Star (LWS) program.

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