forked from eggy/eifueo
phys: geosync and geostationary orbits
This commit is contained in:
parent
09615316d6
commit
7bec6c8eb5
@ -617,6 +617,10 @@ $$\vec{F}_G=\Sigma\vec{F}_c$$
|
|||||||
So the orbital speed of a satellite must be independent of its own mass, such that:
|
So the orbital speed of a satellite must be independent of its own mass, such that:
|
||||||
$$v=\sqrt{\frac{GM}{r}}$$
|
$$v=\sqrt{\frac{GM}{r}}$$
|
||||||
|
|
||||||
|
A **geosynchronous** orbit is one that returns to its original position relative to the orbitee after one rotation of the orbitee.
|
||||||
|
|
||||||
|
A **geostationary** orbit is a geosynchronous orbit that always remains in the same position relative to the orbitee.
|
||||||
|
|
||||||
## Resources
|
## Resources
|
||||||
|
|
||||||
- [IB Physics Data Booklet](/resources/g11/ib-physics-data-booklet.pdf)
|
- [IB Physics Data Booklet](/resources/g11/ib-physics-data-booklet.pdf)
|
||||||
|
Loading…
Reference in New Issue
Block a user