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Launch and Early Orbit phase

In spacecraft operations, Launch and Early Orbit Phase (LEOP) is one of the most critical phases of a mission. Spacecraft operations engineers take control of the satellite after it separates from the launch vehicle. LEOP generally concludes once the satellite is safely positioned in its final orbit.

During this period, operations staff work typically 24 hours a day to activate, monitor and control the various subsystems of the satellite, including the deployment of any satellite appendages (such as antennas, solar arrays, reflectors, and radiators), and undertake critical orbit and attitude control manoeuvres. Extra support staff are typically on hand and on-call during LEOP, relative to staffing during normal operations.

For geostationary satellites, the launch vehicle typically carries the spacecraft to Geostationary Transfer Orbit, or GTO. From this elliptical orbit, the LEOP generally includes a sequence of apogee engine firings to reach the circular geostationary orbit.

See also edit

References edit

  • ESA Spacecraft Operations website

launch, early, orbit, phase, spacecraft, operations, launch, early, orbit, phase, leop, most, critical, phases, mission, spacecraft, operations, engineers, take, control, satellite, after, separates, from, launch, vehicle, leop, generally, concludes, once, sat. In spacecraft operations Launch and Early Orbit Phase LEOP is one of the most critical phases of a mission Spacecraft operations engineers take control of the satellite after it separates from the launch vehicle LEOP generally concludes once the satellite is safely positioned in its final orbit During this period operations staff work typically 24 hours a day to activate monitor and control the various subsystems of the satellite including the deployment of any satellite appendages such as antennas solar arrays reflectors and radiators and undertake critical orbit and attitude control manoeuvres Extra support staff are typically on hand and on call during LEOP relative to staffing during normal operations For geostationary satellites the launch vehicle typically carries the spacecraft to Geostationary Transfer Orbit or GTO From this elliptical orbit the LEOP generally includes a sequence of apogee engine firings to reach the circular geostationary orbit See also editGround segment Satellite space segmentReferences editESA Spacecraft Operations website Retrieved from https en wikipedia org w index php title Launch and Early Orbit phase amp oldid 1150432695, wikipedia, wiki, book, books, library,

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