Circumference = 2 p R
For R= 6400 km then C=40,000 km - 2s.f. input -> 2 s.f. output
For R = 6378.1363 km then C = 40,075.012 km
Except the 8 s.f. value of R is for the mean equatorial radius. What is the meaning /value/purpose of a mean equatorial circumference calculated to 8 s.f.? It depends on the purpose. It MAY have some meaning somewhere.
g = GM/R2 where G = 6.6720 x 10-11, M= 5.9742 x 1024 kg and R = 6378.1363 km
When is it reasonable to quote g=9.7982429 m s-2 and when is it not reasonable?
If you quote 5,6,... sig figs thenyou need to be sure that you have included ALL of the effects that apply at that level of accuracy. For example, if you are doing a satellite trajectory problem and you want 9 sig fig accuracy (e.g. a 4 billion dollar communications satellite or to get to Mars or Pluto) then are you taking into account atmospheric drag, higher-order gravity fields, magnetic torquing, perturbations from the Sun, Moon, etc - and other effects that contribute to the acceleration of the object. Otherwise it is not just unnecessary to quote the extra sig figs - it is dishonest.
What is the altitude above the surface of the Earth where is g 90% of the surface value?
Let's call 0.9 g = g90 and the radius where this is the local gravitational acceleration R90.
Method A - For earth we have g = 9.80 m s-2 so that g90 = 8.82 m s-2
Then R90 = (GM/g90)1/2 = 6719.2 km
The altitude where g is 90% of the surface value is then R90 - R = 6719.2 - 6378.1 = 341 km
Method B - Alternatively, we could simplify the problem - with a little algebra.
0.90 = g90 / g = [ GM / R902 ] / [GM/R2] = [R/R90]2
R90 = R / (0.9)1/2 = R x 1.0541 = 6723.1 km
This value of R90 does ot depend on accuracy of G, M, g. And you could apply it to any planetary object.
The altitude is then 0.0541 R = 345 km
Which answer is correct? Which is more accurate? Method A or B?
These two methods have answers that differ in the SECOND sig fig. Check the numbers - I do not think I made a calculator error. One of the answers is clearly way off.
Method B has
So, when doing such calculations I recommend the following: