The increase of contact radius was calculated for each impact, which is ranging from 41%to44%41%to44%
The rest of this section discusses the evidence base for each impact channel in turn.
Densities are calculated from these fluxes using the circular orbit assumption and local spacecraft velocity for each impact.
Once the depth of melting for each impact has been calculated, the pressure and temperature at that depth is determined.
These three parameters (impactor mass, impact velocity and impact angle) and the mass of the target body are determined for each impact in the N-body accretion simulations.
In the following paragraphs, impact assessment results of the two life cycles are discussed in terms of the corresponding normalized unit for each impact category.
More weight is given to the Phase 3 estimate for each impact because the Phase 3 estimate has lower variance than the Phase 2 estimate.
The description of the results is described country-wise for each impact category, followed with a logical discussion in order to support the results.
For each impact simulation, individual yarn strengths are mapped from experimentally obtained yarn strength distributions, resulting in fabric models with spatially non-uniform failure conditions.
The release fractions from the cask to the environment for each impact condition are preliminarily estimated by referring to a proposed methodology from literature.
For each impact in an N-body accretion simulation, the impact angle, impact velocity and the masses of the two bodies involved are used to calculate melt production using the equations listed above.
