Difference between revisions of "Template:OrbitVelocity/Core"
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m (*renamed Parameter Table to Parameter table;) |
m (Use new mass template) |
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<includeonly>{{#expr: <!-- | <includeonly>{{#expr: <!-- | ||
--> ( <!-- | --> ( <!-- | ||
− | --> {{G}} * {{#if: {{{2|}}}{{#if: {{{b|}}}||1}}|{{{2}}}|{{Body data|{{{b}}} | + | --> {{G}} * {{#if: {{{2|}}}{{#if: {{{b|}}}||1}}|{{{2}}}|{{Body data/Mass|{{{b}}}}}}} / {{OrbitAltitude/Core|{{{1|}}}|{{{2|}}}|0|b={{{b|}}}|pf={{{pf|}}}}} <!-- |
--> ) ^ 0.5 {{#switch: {{{f|}}} | --> ) ^ 0.5 {{#switch: {{{f|}}} | ||
|k=/1000 | |k=/1000 |
Latest revision as of 11:38, 12 May 2018
# | Optional | Description | Default |
---|---|---|---|
1 | No | Period of the orbit in seconds | |
2 | No | Mass of central body in kilograms | |
3 | Yes | Round to the number of decimal places. | Doesn't round |
f | Yes | Factor in which the velocity should be shown. Available values: None (m/s), k (km/s), M (Mm/s), G (Gm/s). | None |
b | Yes | Uses the sidereal rotation period, mass and radius as default from the given body. Can be overwritten. | Not set (makes the first two parameters mandatory) |
pf | Yes | Multiplies the period with this value. Useful to easily calculate semi-synchronous orbits (pf=1/2 then). | 1 |