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From Chris Jones:
The shuttle's so-called direct insertion trajectory puts it into an "orbit" with a perigee around 30 miles and an apogee above 200 miles. This is not an orbit that will last even twice around the earth, which is the reason for the OMS burn performed at first apogee to raise the perigee safely out of the dense atmosphere. Even the reentry burn doesn't really take a spacecraft out of orbit; it lowers the perigee so low (around 20 - 30 miles) that the frictional losses quickly do the rest and take the spacecraft out of orbit. requote: "Even the reentry burn doesn't really take a spacecraft out of orbit" Now that I think about it, the actual _deorbit_burn doesn't take place until the tiles start getting red hot. Ha! ~ CT |
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