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  2. Orbital maneuver - Wikipedia

    en.wikipedia.org/wiki/Orbital_maneuver

    In orbital mechanics, the Hohmann transfer orbit is an elliptical orbit used to transfer between two circular orbits of different altitudes, in the same plane. The orbital maneuver to perform the Hohmann transfer uses two engine impulses which move a spacecraft onto and off the transfer orbit.

  3. LauncherOne - Wikipedia

    en.wikipedia.org/wiki/LauncherOne

    LauncherOne was a two-stage orbital launch vehicle developed and flown by Virgin Orbit that had operational flights from 2021 to 2023, after being in development from 2007 to 2020.

  4. File:Turner's orbit 3.pdf - Wikipedia

    en.wikipedia.org/wiki/File:Turner's_orbit_3.pdf

    Endorse this file for transfer by adding |human=<your username> to this Template.; If this file is freely licensed, but otherwise unsuitable for Commons (e.g. out of Commons' scope, still copyrighted in the US), then replace this Template with {{Do not move to Commons|reason=<Why it can't be moved>}}

  5. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets.

  6. Dynex Semiconductor - Wikipedia

    en.wikipedia.org/wiki/Dynex_Semiconductor

    The Dynex power semiconductor business was originally established in Lincoln over 50 years ago when it was known as AEI Semiconductors Ltd. At that time, the business introduced some of the first silicon-based power semiconductor components in the world.

  7. Orbit insertion - Wikipedia

    en.wikipedia.org/wiki/Orbit_insertion

    In spaceflight an orbit insertion is an orbital maneuver which adjusts a spacecraft’s trajectory, allowing entry into an orbit around a planet, moon, or other celestial body. [1] An orbit insertion maneuver involves either deceleration from a speed in excess of the respective body's escape velocity , or acceleration to it from a lower speed.

  8. Saturn IB - Wikipedia

    en.wikipedia.org/wiki/Saturn_IB

    AS-206, 207, and 208 inserted the Command and Service Module in a 150-by-222-kilometer (81-by-120-nautical-mile) elliptical orbit which was co-planar with the Skylab one. The SPS engine of the Command and Service Module was used at orbit apogee to achieve a Hohmann transfer to the Skylab orbit at 431 kilometers (233 nautical miles). [8]

  9. ION Satellite Carrier - Wikipedia

    en.wikipedia.org/wiki/ION_Satellite_Carrier

    ION Satellite Carrier (formerly ION CubeSat Carrier) is a satellite platform developed, manufactured, and operated by Italian company D-Orbit.The platform features a customizable 64U satellite dispenser capable of hosting a combination of CubeSats that fits the volume.

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