Difference between revisions of "Template:OrbitAltitude"

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m (Fix line breaks (?).)
m (Fix equation (pi^2, not pi^3).)
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-->            ( <!--
 
-->            ( <!--
 
-->                {{{period_s}}}^2 * 6.6726e-11 * {{{mass_kg}}} <!--
 
-->                {{{period_s}}}^2 * 6.6726e-11 * {{{mass_kg}}} <!--
-->                / (4 * pi^3) <!--
+
-->                / (4 * pi^2) <!--
 
-->            ) ^ (1/3) <!--
 
-->            ) ^ (1/3) <!--
 
-->        ) / 1000 <!--
 
-->        ) / 1000 <!--
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! Usage || Produces
 
! Usage || Produces
 
|-
 
|-
| <pre><nowiki>{{OrbitAltitude | period_s=86400 | mass_kg=4.515e21 | radius_km=320}}</nowiki></pre> || {{OrbitAltitude | period_s=86400 | mass_kg=4.515e21 | radius_km=320}}
+
| <pre><nowiki>{{OrbitAltitude | period_s=64980 | mass_kg=4.515e21 | radius_km=320}}</nowiki></pre> || {{OrbitAltitude | period_s=64980 | mass_kg=4.515e21 | radius_km=320}}
 
|}
 
|}
  

Revision as of 23:15, 15 October 2012

Expression error: Unrecognized punctuation character "{". km

Usage Produces
{{OrbitAltitude | period_s=64980 | 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).