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
Name | Description |
---|---|
Meteors | Computes the fluence for meteoroid particulates. |
Debris | Computes the fluence for debris particulates. |
Meteor Damage | Computes the fluence for meteoroid particulates that cause damage. |
Debris Damage | Computes the fluence for debris particulates that cause damage. |
Data Provider Elements
Name | Dimension | Type | Description |
---|---|---|---|
Impact mass fluence | MassPerArea | Real Number or Text | The 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 mass | Mass | Real Number or Text | The 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 fluence | Fluence | Real Number or Text | The 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). |
Impacts | Unitless | Real Number or Text | The 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. |