Difference between revisions of "Template:OrbitAltitude"
From Kerbal Space Program Wiki
(Make a template for calculating the altitude of an orbit with the given period, planet mass, and planet radius.) |
m (Fix line breaks (?).) |
||
Line 1: | Line 1: | ||
− | {{#expr: | + | {{#expr: <!-- |
− | ( | + | --> ( <!-- |
− | ( | + | --> ( <!-- |
− | ( | + | --> ( <!-- |
− | {{{period_s}}}^2 * 6.6726e-11 * {{{mass_kg}}} | + | --> {{{period_s}}}^2 * 6.6726e-11 * {{{mass_kg}}} <!-- |
− | / (4 * pi^3) | + | --> / (4 * pi^3) <!-- |
− | ) ^ (1/3) | + | --> ) ^ (1/3) <!-- |
− | ) / 1000 | + | --> ) / 1000 <!-- |
− | ) - {{{radius_km}}} | + | --> ) - {{{radius_km}}} <!-- |
− | }} km<noinclude> | + | --> }} km<noinclude> |
{| class="wikitable" | {| class="wikitable" |
Revision as of 23:10, 15 October 2012
Expression error: Unrecognized punctuation character "{". km
Usage | Produces |
---|---|
{{OrbitAltitude | period_s=86400 | mass_kg=4.515e21 | radius_km=320}} |
0.00 m |
This template calculates the altitude of an orbit, given the mass of the planet (in kg), the planet's radius (in km), and the period of the orbit (in seconds).