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Ballistic limit equation (BLE) is an important tool for spacecraft shield design.
A variety of different ballistic limit equations (BLEs) have been developed for many different types of structural wall configurations.
The outcome of projectile impacts on spaced aluminium armour (i.e. Whipple shield) at hypervelocity is traditionally predicted by semi-analytical equations known as ballistic limit equations (BLEs).
The experimental results were used to develop and validate a new empirical Ballistic Limit Equation (BLE), which was derived from an existing Whipple-shield BLE.
Typical orbital debris risk analyses that include ballistic limit equations (BLEs) and curves (BLCs) assume that orbital debris particles are spherical in shape.
Traditional protective shield design consists of a "bumper" that is placed at a relatively small distance away from the main "inner wall" of the spacecraft component, the performance of which is typically characterized by its ballistic limit equation (BLE).
This new assessment methodology is based on triple-wall ballistic limit equations (BLEs), specifically the Schäfer-Ryan-Lambert (SRL) BLE, which is applicable for describing failure threshold levels for satellite components following a hypervelocity impact.
The proposed method combines a debris flux model with the Schäfer Ryan Lambert ballistic limit equation (BLE), which accounts for the inherent shielding of components positioned behind the spacecraft structure wall.
Orbital debris risk assessments for the Orion vehicle, as well as the Shuttle, Space Station and other satellites use ballistic limit equations (BLEs) that have been developed using high speed impact test data and results from numerical simulations that have used spherical projectiles.
Based on a study combining hypervelocity impact testing and hydrodynamic impact simulations on multiple shield configurations including non-parallel first and rear walls, this paper provides equation adjustments for use with the double wall Ballistic Limit Equation (BLE) for a variety of impact speeds, non-parallel wall angles and impact obliquities.
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