Satellite: Astrogator Maneuver Ephemeris Block Initial: SEET

Not defined for this class of object.

Name Dimension Type Description
Time DateFormat Real Number Time.
DamageFlux Flux Real Number The total impact flux that cause damage, from all meteoroid particulates, found as a simple sum of the damaging impact flux of all particulates.
DamageMassFlux MassFlux Real Number The total impact mass flux that cause damage, from all meteoroid particulates, found as the integral of the damaging particle impact flux distribution with respect to mass.
GeoMagFieldDipoleL Unitless Real Number The L value for the field line passing through the vehicle's location computed using the dipole approximation to the magnetic field.
GeoMagFieldFieldLineSeparation AngleUnit Real Number The centric angle between the north footprint of the field line containing the vehicle's location and the north footprint of the field line containing the target's location. The north footprint is the point of intersection of the field line with the earth's surface north of the magnetic equator. If either north footprint is not defined, then the south footprint is used.
ImpactFlux Flux Real Number The total impact flux from all meteoroid particulates, found as a simple sum of the impact flux of all particulates.
ImpactMassFlux MassFlux Real Number The total impact mass flux from all meteoroid particulates, found as the integral of the particle impact flux distribution with respect to mass.
SAAFluxIntensity FluxIntensity Real Number The SAA flux intensity at the vehicle's location for the vehicle's channel specification.
VehicleTemperature Temperature Real Number Vehicle temperature, computed assuming thermal equilibrium.

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