Data Provider Groups | Data Provider Elements

SEET Particle Fluence

Computes the total fluence (i.e., the total flux of all particulates integrated over time). Valid for vehicles whose central body is earth.

Available for these objects: LaunchVehicle, Missile, Satellite

Type: Interval data given specified evaluation intervals and step sizes. Intended to be used only with elements from this same data provider.

Availability: Reports | Graphs

Data Provider Groups

NameDescription
MeteorsComputes the fluence for meteoroid particulates.
DebrisComputes the fluence for debris particulates.
Meteor DamageComputes the fluence for meteoroid particulates that cause damage.
Debris DamageComputes the fluence for debris particulates that cause damage.

Data Provider Elements

NameDimensionTypeDescription
Impact mass fluenceMassPerAreaReal Number or TextThe total impact mass flux from all particulates (found as the integral of the particle impact flux distribution with respect to mass) integrated over the requested time interval. The integration is performed using Simpson's rule using a step size based upon the specified step size, adjusted to insure that an even number of steps is taken (as is required for Simpson's rule to be used).
Impact massMassReal Number or TextThe total mass impinging the spacecraft over the requested time interval. This is found by multiplying the cross sectional area by the impact mass fluence.
Impact fluenceFluenceReal Number or TextThe total impact flux from all particulates (found as a simple sum of the impact flux of all particulates) integrated over the requested time interval. The integration is performed using Simpson's rule using a step size based upon the specified step size, adjusted to insure that an even number of steps is taken (as is required for Simpson's rule to be used).
ImpactsUnitlessReal Number or TextThe total number of impacts impinging the spacecraft over the requested time interval. This is found by multiplying the cross sectional area by the impact fluence.