Period charge
Posted: 02.07.2008, 15:51
http://en.wikibooks.org/wiki/Celestia/SSC_File
CHARGE
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For a closed, elliptical orbit around our Sun,
P = sqrt (( q / ( 1 - e)) ^3)
or = a^1.5
When defining an hyperbolic orbit around our Sun, set period to be
P = sqrt (( q / ( e - 1)) ^3)
CHARGE
Code: Select all
For a closed, elliptical orbit around our Sun,
P = ( q / ( 1 - e)) ^1,5
or = a^1.5
When defining an hyperbolic orbit around our Sun, set period to be
P = ( q / ( e - 1)) ^1,5