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    PREPARATION OF THE KENTUCKY RE-ENTRY UNIVERSAL PAYLOAD SYSTEM FOR ORBITAL FLIGHT

    Nichols, J. / Dietz, C. / Sparks, J. et al. | British Library Conference Proceedings | 2019

    Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7

    Rowe, J. / Smith, S. | British Library Conference Proceedings | 2007

    Development of a Novel Low Stored Volume High-Altitude Wing Design

    Kudva, J. / Scott, M. / Jacob, J. et al. | British Library Conference Proceedings | 2009

    Corrosion detection and assessment in gas distribution pipes

    Burd, J. / Smith, S. | Tema Archiv | 2000

    Aeroelastic Deformation and Buckling of Inflatable Wings under Dynamic Loads AIAA Paper 2007-2239 CD-ROM Number 7

    Simpson, A. / Rowe, J. / Smith, S. et al. | British Library Conference Proceedings | 2007

    Effect of Boundary Conditions on Geometric Control for an Inflatable Pathfinder System

    Fulcher, J. / Smith, S. / Baker, J. et al. | British Library Conference Proceedings | 2014

    AIAA-2004-1503 Development of UV-Curable Inflatable Wings for Low-Density Flight Applications

    Smith, S. / Scarborough, S. / Smith, T. et al. | British Library Conference Proceedings | 2004

    Designing Collaborative Automated Planners for Agile Adaptation to Dynamic Change

    Truxler, R. / Roth, E. / Scott, R. et al. | British Library Conference Proceedings | 2012

    Parametric response of thin beams and film strips in a vacuum

    Vulkarni, V. / Smith, S. / Main, J. | AIAA | 2001

    BIG BLUE II: Mars Aircraft Prototype with Inflatable-Rigidizable Wings

    Simpson, A. / Jacob, J. / Smith, S. et al. | British Library Conference Proceedings | 2005

    EVA - Don't Leave Earth Without It

    Cupples, J. / Smith, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    Simulation of Deployment Dynamics of an Inflatable Solar Array

    Clem, A. / Smith, S. / Main, J. | British Library Conference Proceedings | 1999

    Post-flight testing and analysis of zero-gravity deployment of an inflating tube

    Smith, S. / Elliott, M. / Main, J. et al. | AIAA | 2001

    A new class of high speed disconnect switch based on piezoelectric actuators

    Graber, L. / Smith, S. / Soto, D. et al. | IEEE | 2015

    Design Limitations of Deployable Wings for Small Low Altitude UAVS

    Jacob, J. / Smith, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

      Design Limitations of Deployable Wings for Small Low Altitude UAVs

      Jacob, J. / Smith, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    Altitude Comparison Technique Using the MC-130H APN-232 RADAR Altimeter

    Armstrong, J. / Smith, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Design of HALE Aircraft Using Inflatable Wings

    Jacob, J. / Smith, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008