Versions Compared

Key

  • This line was added.
  • This line was removed.
  • Formatting was changed.
Comment: Migration of unmigrated content due to installation of a new plugin
Composition Setup

By navigating to the site http://spaceflight.nasa.gov/realdata/tracking/ you can obtain tracking information giving the altitude and speed of the international space stationInternational Space Station (ISS). Suppose that the information displayed on the site was as shown in the screen capture above. By making the assumption that the space station's orbit is a circle with its center at the center of the earth,

Excerpt

find the approximate magnitude of the acceleration experienced by the space station as a result of the gravitational pull of the earth.

Solution

Toggle Cloak
idsys
System:
Cloak
idsys

The ISS will be treated as a point particle.
Cloak
sys
sys

Toggle Cloak
idint
Interactions:
Cloak
idint

External influence from the earth (gravity).
Cloak
int
int

Toggle Cloak
idmod
Model:
Cloak
idmod

Uniform Circular Motion.
Cloak
mod
mod

Toggle Cloak
idapp
Approach:

Cloak
idapp

Based upon the assumption of uniform circular motion, the acceleration of the ISS must satisfy:

Latex
\begin{large}\[ a = \frac{v^{2}}{r} \] \end{large}

We know that v = 7699.59 m/s, but r requires some thought. The altitude of 346450 m is not the full radius of the orbit, it is only the height of the ISS above the surface of the earth. To find the full orbital radius, we must add on the earth's radius. The earth's radius can be found on the web or in a number of books to be Re = 6,380,000 m. Thus, the orbital radius is r = 6,730,000 m. With this determined, we find:

Latex
\begin{large} \[ a = \mbox{8.81 m/s}^{2} \] \end{large}
Note

Earth's gravity is not insignificant at level of the ISS's orbit. If it was, the ISS would just fly off into space!

Cloak
app
app