The MOONRISE-payload as proof of principle for mobile selective laser melting of lunar regolith
The Leo Particulate Environment as Determined by LDEF
Structure-borne Noise Prediction Using an Energy Finite Element Method
Space Shuttle Meteoroid and Orbital Debris Impact Damage (IAA 00-6.4.03)
Preliminary Analysis of LDEF Instrument A0187-1, The Chemistry of Micro-Meteoroids Experiment (CME)
Prediction and Verification of Energy Flow in a Structure Using an Energy Finite Element Approach
Powertrain Sound Power Measurement Using a Two-Degree-of-Freedom Positioning Mechanism
Parametrischer Bauraum - synchronisierter Fahrzeugentwurf
Natural and Orbital Debris Particles on LDEF's Trailing and Forward-Facing Surfaces
M/OD Impacts on the Multipurpose Logistics Module: Post Flight Inspection Results
Measuring Track Densities in Lunar Grains Using Image Analysis
Measuring Track Densities in Lunar Grains Using Image Analysis
Geraeusche und Esrchuetterungen als mechanische Schwingungen infolge Eisenbahn- und Strassenverkehr
Dealing with Conflicting Information: Will Crews Rely on Automation?
Cratering and Penetration Experiments in Teflon Targets at Velocities from 1 To 7 KM/S
Assessment of high velocity impacts on exposed Space Shuttle surfaces
Analytical Electron Microscopy of LDEF Impactor Residues
Active Control of Wind Noise Using Robust Feedback Control