Launch Azimuth

From OrbiterWiki
Revision as of 22:32, 25 October 2006 by Kwan3217 (talk | contribs)
Jump to navigation Jump to search

The launch azimuth is the angle between north direction and the projection of the initial orbit plane onto the launch location.

Relation between latitude and inclination

Not all inclinations can be reached at a position on a celestial body. The problem is, that the launch location has to be a point inside the target orbit plane. So, if the latitude of a launch location is higher than the inclination, the orbit can't be reached directly.

Using spherical trigonometry, we can calculate the launch azimuth required to hit any allowed orbit inclination.

where is the desired orbit inclination, is the launch site latitude, and is the launch azimuth. Solving for azimuth:

This shows mathematically why the inclination must be greater than the launch latitude: Otherwise, the argument to the inverse sine function would be greater than 1, which is out of its domain. Therefore there is no solution in this case.

Example: The International Space Station orbits at 51.6° inclination. A space shuttle launching from Cape Canaveral (latitude 28.5°) needs to travel at what azimuth?

As a launch on the southeastern course would overfly the Bahamas, Cuba, and South America, the northeastern course is always used. This is ocean all the way to Ireland.

A launch from Baikonur Cosmodrome (latitude 45.9°) to the same orbit requires an azimuth of

Launch again is always on the northeastern course. Both courses are over thousands of km of land, but some land belowe the course to the northeast has been reserved as the first-stage impact area.

This article is a stub. You can help Orbiterwiki by expanding it.