Missile: SEET Particle Fluence: Debris

Computes the fluence for debris particulates.

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 MassUnit 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.

STK Programming Interface 11.0.1