theotherguy
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I recentley got accepted as a NASA high school aerospace scholar. This is a special program hosted by NASA in which thousands of students from across the country submit an essay and a transcript to senators, who then select the top students to compete in a rigourous program designed to prime students for aerospace engineering.
I am supposed to do ten long and complicated projects over the course of the year and then attend a summer program with a select group of students and discuss with NASA scientists the probelms facing space travel.
However, I have done all of my first project except for this one question, which I simply don't know how to answer. I recognize it as a simple acceleration equation, but it has some terms that I don't quite understand, as we havent covered orbits in my physics class yet. My physics teacher is out on a holiday and none of my peers know how to do this either. Can anyone help me understand how to do this problem?
I'm sorry if I sound lazy, but I've been looking up information on how to do this for some time and I can't seem to figure it out.
I am supposed to do ten long and complicated projects over the course of the year and then attend a summer program with a select group of students and discuss with NASA scientists the probelms facing space travel.
However, I have done all of my first project except for this one question, which I simply don't know how to answer. I recognize it as a simple acceleration equation, but it has some terms that I don't quite understand, as we havent covered orbits in my physics class yet. My physics teacher is out on a holiday and none of my peers know how to do this either. Can anyone help me understand how to do this problem?
Part Two: Shuttle Math The De-orbit Burn
When it is time for the Space Shuttle to come in for a landing, it needs to reenter the Earth's atmosphere at the right time and place so that it can land successfully at the designated landing strip (Kennedy Space Center in Florida, Edwards Air Force Base in California, or the White Sands Test Facility in New Mexico).
Depending on the Shuttle's altitude, it's de-orbit burn must occur for the correct length of time for the Shuttle to begin its descent at the right speed and in the correct location. The de-orbit burn is done against the direction of travel. The Shuttle keeps going in the same direction but slows down due to the drag on the spacecraft as it enters the atmosphere.
De-orbit maneuvers are usually done to lower the perigee of the orbit to 60 miles (or less). The Orbiter is captured and re-enters as it passes into the atmosphere at this altitude.
There is a change of 1 mile for every 2 feet per second (fps) change in velocity when you are below a 500-mile altitude above the Earth.
Determine the change in velocity (delta-V) that the Shuttle will need to make if it is at an altitude of 220 miles above the Earth at apogee and 215 miles above the Earth at perigee, and needs to drop the perigee to an altitude of 60 miles.
I'm sorry if I sound lazy, but I've been looking up information on how to do this for some time and I can't seem to figure it out.