Posted 19 June 2005 - 07:33 PM
When it is time for the space shuttle to come in for a landing, it needs to re-enter the Earth's atmosphere at the right time and place so that it can land successfully at the designated landing strip. Depending on the shuttle's altitude, its deorbit burn must occur for the correct length of time in order for the shuttle to begin its descent at the right speed and in the correct location. The deorbit burn is done against the direction of travel. The shuttle keeps moving in the same direction, but it slows down due to the drag on the spacecraft as it enters the atmosphere. Deorbit maneuvers are usually done to lower the perigee of the orbit to 60 miles (or less). The orbiter will get captured and will re-enter as it passes into the atmosphere of this altitude.
Question :
Calculate the change in velocity (in m/s) that must be used to lower the perigee from 230 miles to a
60 mile altitude? To reduce the shuttle altitude by 1 mile there must be 1 foot per second chane in velocity. (1 f = 0.31m)
Help would be much appreciated
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