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    Mars 2020 ECAM Imaging System Initial Results

    Williams, N. R. / Lambert, M. / Algermissen, S. et al. | NTRS | 2021

    Adaptive control of flexible systems

    Free access
    Lambert, M / Lambert, Martin | BASE | 2016

    Simulation of a Mars Aerocapture Vehicle on Flow Adapted Unstructured Grids with the DLR TAU Code

    Potter, D. / Karl, S. / Lambert, M. et al. | British Library Conference Proceedings | 2012

    CFD Modelling of Re-Entry Flows Including Gas Radiation

    Karl, S. / Lambert, M. / European Space Agency | British Library Conference Proceedings | 2011

    North East Aircraft Museum : New England Air Museum, Aviation, RAF Usworth

    Surhone, Lambert M. | SLUB | 2010
    Contributors: Surhone, Lambert M.

    Improving the Significance of MM/SD Risk Analysis by Application of the SRL Ballistic Limit Equation

    Schafer, F. / Putzar, R. / Ryan, S. et al. | British Library Conference Proceedings | 2009

    CFD Analysis of Radiative Heat Loading on Hypervelocity Re-Entry Vehicles

    Karl, S. / Lambert, M. / American Institute of Aeronautics and Astronautics; DUR; Deutsche Gesellschaft fur Luft- und Raumfahrt | British Library Conference Proceedings | 2009

    Modelling of flawed riveted structures for EC inspection in aeronautics

    Paillard, S. / Pichenot, G. / Lambert, M. et al. | Tema Archive | 2008

    A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures

    Ryan, S. / Schaefer, F. / Destefanis, R. et al. | Elsevier | 2007

    A 3D model for eddy current inspection in aeronautics. Application to riveted structures

    Paillard, S. / Pichenot, G. / Lambert, M. et al. | Tema Archive | 2007

    Automotive Adsorption Air Conditioner Powered by Exhaust Heat. Part 1: Conceptual and Embodiment Design

    Lambert, M A / Jones, B J | SAGE Publications | 2006

    Automotive Adsorption Air Conditioner Powered by Exhaust Heat. Part 2: Detailed Design and Analysis

    Lambert, M A / Jones, B J | SAGE Publications | 2006

    Eddy current modelling for fasteners inspection in aeronautic

    Paillard, S. / Pichenot, G. / Lambert, M. et al. | Tema Archive | 2006

    Analysis of the Potentialities and Limitations of the Integration between the IMSA and the Level Set Method for Inverse Scattering

    Benedetti, M. / Lesselier, D. / Massa, A. et al. | British Library Conference Proceedings | 2006

    An excitation function for hypervelocity impact-induced wave propagation in satellite structures

    Ryan, S. / Schäfer, F. / Spencer, G. et al. | AIAA | 2006

    Experimental and numerical study to investigate impact-induced wave propagation in spacecraft

    Schäfer, F. / Spencer, G. / Ryan, S. et al. | AIAA | 2006

    Vulnerability of Spacecraft Electronics Boxes to Hypervelocity Impacts (IAC-05-B6.4.02)

    Putzar, R. / Schafer, F. K. / Stokes, H. et al. | British Library Conference Proceedings | 2006

    VULNERABILITY OF SHIELDED FUEL PIPES AND HEAT PIPES TO HYPERVELOCITY IMPACTS

    Putzar, R. / Schafer, F. / Romberg, O. et al. | British Library Conference Proceedings | 2005

    HYPERVELOCITY IMPACT TESTING OF CFRP/AL HONEYCOMB SATELLITE STRUCTURES

    Schafer, F. / Destefanis, R. / Ryan, S. et al. | British Library Conference Proceedings | 2005

    DEBRIS SHIELDING DEVELOPMENT FOR THE ATV INTEGRATED CARGO CARRIER

    Destefanis, R. / Lambert, M. / Schafer, F. et al. | British Library Conference Proceedings | 2005

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