The EMI light-gas gun acceleration facilities available for the simulation of micrometeoroid/orbital debris impact, as well as high-speed diagnostic installations and special instrumentation to visualize hypervelocity impact phenomena, are described. Using this equipment, various bumper shield arrangements have been tested in a wide range of particle masses and impact velocities, within the frame of the COLUMBUS Meteoroid/Debris Protection Study (MDPS), presently performed by ESA-ESTEC. Some recent essential results are presented. They demonstrate the effectiveness, but also the limitations and constraints of bumper shield protection systems
The increasing amount of debris in Earth orbit poses a danger to users of the orbital environment. D...
International audienceThe meteoroids and debris environment play an important role in the reduction ...
This work presents a comprehensive numerical study of two foils protection shield configuration agai...
Space vehicles, operating on a long-term basis, need to be protected against meteoroid and space deb...
Long-term space flight activities in low earth orbit are confronted with the increasing threat of or...
Space environmental conditions are developing in a way that protection of space vehicles is becoming...
The ESA laboratory module Columbus, part of the NASA space station Freedom, has to be protected agai...
Modern acceleration equipment is used to simulate orbital debris interaction with space vehicle comp...
Activities at EMI in the field of hypervelocity impact techniques are reported. Optimization experim...
An experimental impact simulation is currently performed with respect to Columbus hull components. T...
A relatively simple shock analysis is developed for hypervelocity impact onto spacecraft bumpers. Th...
A series of experiments has been performed on the Sandia HyperVelocity Launcher (HVL) to evaluate th...
The computational technique of Smoothed Particle Hydrodynamics (as implemented in the hydrocodes AUT...
The paper gives a short survey of the historical development of the EMI and the Terminal Ballistics ...
AbstractAs the orbital debris population continues to grow significant tangible threats to robotic a...
The increasing amount of debris in Earth orbit poses a danger to users of the orbital environment. D...
International audienceThe meteoroids and debris environment play an important role in the reduction ...
This work presents a comprehensive numerical study of two foils protection shield configuration agai...
Space vehicles, operating on a long-term basis, need to be protected against meteoroid and space deb...
Long-term space flight activities in low earth orbit are confronted with the increasing threat of or...
Space environmental conditions are developing in a way that protection of space vehicles is becoming...
The ESA laboratory module Columbus, part of the NASA space station Freedom, has to be protected agai...
Modern acceleration equipment is used to simulate orbital debris interaction with space vehicle comp...
Activities at EMI in the field of hypervelocity impact techniques are reported. Optimization experim...
An experimental impact simulation is currently performed with respect to Columbus hull components. T...
A relatively simple shock analysis is developed for hypervelocity impact onto spacecraft bumpers. Th...
A series of experiments has been performed on the Sandia HyperVelocity Launcher (HVL) to evaluate th...
The computational technique of Smoothed Particle Hydrodynamics (as implemented in the hydrocodes AUT...
The paper gives a short survey of the historical development of the EMI and the Terminal Ballistics ...
AbstractAs the orbital debris population continues to grow significant tangible threats to robotic a...
The increasing amount of debris in Earth orbit poses a danger to users of the orbital environment. D...
International audienceThe meteoroids and debris environment play an important role in the reduction ...
This work presents a comprehensive numerical study of two foils protection shield configuration agai...