Ballistic limit equations (BLEs) are used for the damage prediction of spacecraft in a meteoroid and space debris environment. For double-wall configurations, the Cour-Palais/Christiansen equations have been modified to yield a general approach including the influence of the shield thickness. The ratio of shield thickness to particle diameter is considered as additional parameter in the equations. These equations result in the single-wall equation when the shield thickness approaches zero. The modifications can also be applied to other BLEs. Impact tests have been performed in order to validate the modified equations. In this paper, the test results are compared to the modified BLEs. Especially in the hypervelocity region, the new equations...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
During a recent experimental test campaign performed in the framework of ESA Contract 16721, the bal...
All earth-orbiting spacecraft are susceptible to impacts by orbital debris particles, which can occu...
All Earth-orbiting spacecraft are susceptible to damage that can be caused by high-speed impacts wit...
The fundamental components of any meteoroid/orbital debris (MOD) risk assessment calculation are env...
All earth-orbiting spacecraft are susceptible to impacts by orbital debris particles, which can occu...
One of the major design considerations of earth-orbiting spacecraft is the damage that might occur f...
A new ballistic limit equation has been developed for the case of a Whipple shield configuration or ...
A new ballistic limit equation has been developed for the case of a Whipple shield configuration or ...
Ballistic limit curves (BLCs) for dual- or multi-wall spacecraft wall systems impacted by spherical ...
AbstractThe parallel, Double Wall, hypervelocity impact shield configuration has been heavily tested...
The fundamental components of any micrometeoroid and orbital debris (MMOD) risk assessment are MMOD ...
It has been known that space debris or meteoroid impact damage can have significant effects on space...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
During a recent experimental test campaign performed in the framework of ESA Contract 16721, the bal...
All earth-orbiting spacecraft are susceptible to impacts by orbital debris particles, which can occu...
All Earth-orbiting spacecraft are susceptible to damage that can be caused by high-speed impacts wit...
The fundamental components of any meteoroid/orbital debris (MOD) risk assessment calculation are env...
All earth-orbiting spacecraft are susceptible to impacts by orbital debris particles, which can occu...
One of the major design considerations of earth-orbiting spacecraft is the damage that might occur f...
A new ballistic limit equation has been developed for the case of a Whipple shield configuration or ...
A new ballistic limit equation has been developed for the case of a Whipple shield configuration or ...
Ballistic limit curves (BLCs) for dual- or multi-wall spacecraft wall systems impacted by spherical ...
AbstractThe parallel, Double Wall, hypervelocity impact shield configuration has been heavily tested...
The fundamental components of any micrometeoroid and orbital debris (MMOD) risk assessment are MMOD ...
It has been known that space debris or meteoroid impact damage can have significant effects on space...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
One of the primary design considerations of earth-orbiting spacecraft is the mitigation of the damag...
During a recent experimental test campaign performed in the framework of ESA Contract 16721, the bal...