Simulation of a Mars Aerocapture Vehicle on Flow Adapted Unstructured Grids with the DLR TAU Code
CFD Modelling of Re-Entry Flows Including Gas Radiation
North East Aircraft Museum : New England Air Museum, Aviation, RAF Usworth
Improving the Significance of MM/SD Risk Analysis by Application of the SRL Ballistic Limit Equation
CFD Analysis of Radiative Heat Loading on Hypervelocity Re-Entry Vehicles
Automotive Adsorption Air Conditioner Powered by Exhaust Heat. Part 2: Detailed Design and Analysis
Automotive Adsorption Air Conditioner Powered by Exhaust Heat. Part 2: Detailed Design and Analysis
Vulnerability of Spacecraft Electronics Boxes to Hypervelocity Impacts (IAC-05-B6.4.02)
VULNERABILITY OF SHIELDED FUEL PIPES AND HEAT PIPES TO HYPERVELOCITY IMPACTS
DEBRIS SHIELDING DEVELOPMENT FOR THE ATV INTEGRATED CARGO CARRIER
HYPERVELOCITY IMPACT TESTING OF CFRP/AL HONEYCOMB SATELLITE STRUCTURES