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<p>perform various <a href="page.php?w=orbital_maneuver">orbital maneuver</a>s according to requirements of each mission profile: <a href="page.php?w=orbit_insertion">orbital injection</a> after <a href="page.php?w=RS-25">main engine</a> cutoff, orbital corrections during flight, and the final deorbit burn for <a href="page.php?w=atmospheric_entry">reentry</a>. From STS-90 onwards the OMS were typically ignited part-way into the Shuttle's ascent for a few minutes to aid acceleration to orbital insertion. Notable exceptions were particularly high-altitude</p><p>
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