A) where the shuttle begins to use aerodynamics to steer.
B) where a balloon can float no higher
C) where ionic winds dominate over atmospheric winds
D) where 100 km is a height normal to the surface
These don't seem very objective.
How about:
1) Target Planet must have an atmosphere not already collapsed by low temperature.
2) Determine target planet's "metre" according to French Academy of Sciences methodology.
3) Determine representative mass of target planet for a one target planet meter diameter sphere. For earth use something like figure 5
4) Find a height normal above the planet surface.
5) Determine orbital velocity for height in 4) and launch meter object in a circularized orbit.
6) Repeat step 4) and 5) exclusively of prior heights until meter object makes exactly one orbit but impacts planet directly under the launch position. This is the height of the atmosphere or where it ends and space begins.
Call it the Newton Napoleon Atmospheric Height Algorithm or some better title.
B) where a balloon can float no higher
C) where ionic winds dominate over atmospheric winds
D) where 100 km is a height normal to the surface
These don't seem very objective.
How about:
1) Target Planet must have an atmosphere not already collapsed by low temperature.
2) Determine target planet's "metre" according to French Academy of Sciences methodology.
3) Determine representative mass of target planet for a one target planet meter diameter sphere. For earth use something like figure 5
4) Find a height normal above the planet surface.
5) Determine orbital velocity for height in 4) and launch meter object in a circularized orbit.
6) Repeat step 4) and 5) exclusively of prior heights until meter object makes exactly one orbit but impacts planet directly under the launch position. This is the height of the atmosphere or where it ends and space begins.
Call it the Newton Napoleon Atmospheric Height Algorithm or some better title.