Drag model
Acceleration due to atmospheric drag.
Type | Intent | Optional | Attributes | Name | ||
---|---|---|---|---|---|---|
real(kind=wp), | intent(in), | dimension(3) | :: | vrel |
velocity relative to the atmosphere [km/s] |
|
real(kind=wp), | intent(in) | :: | cd |
spacecraft drag coefficient [--] |
||
real(kind=wp), | intent(in) | :: | area |
cross-section area [km^2] |
||
real(kind=wp), | intent(in) | :: | m |
spacecraft mass [kg] |
||
real(kind=wp), | intent(in) | :: | rho |
atmospheric density [kg/km^3] |
||
real(kind=wp), | intent(out), | dimension(3) | :: | acc |
drag acceleration vector [km/s^2] |