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    Adaptive Deployable Entry Placement Technology (ADEPT) Development for Small Sat Class Venus Missions

    Cassell, Alan M. / Wercinski, Paul F. / Venkatapathy, Ethiraj et al. | NTRS | 2018
    Keywords: Spacecraft Design, Testing And Performance

    Studies in Support of Venus Aerocapture Utilizing Drag Modulation

    Beck, Robin / Venkatapathy, Ethiraj / Aftosmis, Michael et al. | NTRS | 2018
    Keywords: Spacecraft Design, Testing And Performance

    Ablators: From Apollo to Future Missions to Moon, Mars and Beyond

    Venkatapathy, Ethiraj | NTRS | 2019
    Keywords: Spacecraft Design, Testing And Performance

    A Discussion of the Need to Sustain Mission Ready TPS and for Continued Development of Innovative Entry System Technologies

    Venkatapathy, Ethiraj / Ellerby, Donald T. / Gasch, Matthew J. et al. | NTRS | 2019
    Keywords: Spacecraft Design, Testing And Performance

    ADEPT Sounding Rocket One (SR-1) Flight Test

    Cassell, Alan / Wercinski, Paul / Venkatapathy, Ethiraj | NTRS | 2019
    Keywords: Spacecraft Design, Testing And Performance

    Development of an Ablative 3D Quartz / Cyanate Ester Composite for the Orion Spacecraft Compression Pad

    Feldman, Jay / Venkatapathy, Ethiraj / Wilkinson, Curt et al. | NTRS | 2015
    Keywords: Spacecraft Design, Testing And Performance

    Ablators - From Apollo to Future Missions to Moon, Mars and Beyond

    Venkatapathy, Ethiraj | NTRS | 2019
    Keywords: Spacecraft Design, Testing And Performance

    Structures and Mechanisms Design Concepts for Adaptive Deployable Entry Placement Technology

    Yount, Bryan C. / Arnold, James O. / Gage, Peter J. et al. | NTRS | 2012
    Keywords: Spacecraft Design, Testing And Performance

    Progress in Payload Separation Risk Mitigation for a Deployable Venus Heat Shield

    Smith, Brandon P. / Yount, Bryan C. / Venkatapathy, Ethiraj et al. | NTRS | 2013
    Keywords: Spacecraft Design, Testing And Performance

    Enabling Venus In-Situ Science - Deployable Entry System Technology, Adaptive Deployable Entry and Placement Technology (ADEPT): A Technology Development Project funded by Game Changing Development Program of the Space Technology Program

    Wercinski, Paul F. / Venkatapathy, Ethiraj / Gage, Peter J. et al. | NTRS | 2012
    Keywords: Spacecraft Design, Testing And Performance

    Transformable and Reconfigurable Entry, Descent and Landing Systems and Methods

    Fernandez, Ian M. / Venkatapathy, Ethiraj / Hamm, Kenneth R. | NTRS | 2014
    Keywords: Spacecraft Design, Testing And Performance

    SPRITE: A TPS Test Bed for Ground and Flight

    Prabhu, Dinesh K. / Agrawal, Parul / Peterson, Keith H. et al. | NTRS | 2012
    Keywords: Spacecraft Design, Testing And Performance

    Development of an Integrated Data Acquisition System for a Small Flight Probe

    Swanson, Gregory T. / Empey, Daniel M. / Skokova, Kristina A. et al. | NTRS | 2012
    Keywords: Spacecraft Design, Testing And Performance

    Ablators for Human and Robotic Exploration of the Moon, Mars and Beyond

    Venkatapathy, Ethiraj / Beck, Robin A. / Gage, Peter J. et al. | NTRS | 2019
    Keywords: Spacecraft Design, Testing And Performance

    ADEPT - A Mechanically Deployable Entry System Technology in Development at NASA

    Venkatapathy, Ethiraj / Wercinski, Paul / Cassell, Alan et al. | NTRS | 2016
    Keywords: Spacecraft Design, Testing And Performance

    Progress Towards Providing Heat-Shield for Extreme Entry Environment Technology (HEEET) for Venus and Other New Frontiers Missions

    Venkatapathy, Ethiraj / Ellerby, Don / Gage, Peter | NTRS | 2017
    Keywords: Spacecraft Design, Testing And Performance

    4.0 Hypersonic Systems

    Venkatapathy, Ethiraj / Munk, Michelle / Powell, Dick et al. | NTRS | 2005
    Keywords: Spacecraft Design, Testing And Performance

    Progress Towards providing Heat-Shield for Extreme Entry Environment Technology (HEEET) for Venus and other New Frontiers Missions

    Venkatapathy, Ethiraj / Ellerby, Don / Gage, Peter | NTRS | 2017
    Keywords: Spacecraft Design, Testing And Performance

    Shuttle Orbiter Contingency Abort Aerodynamics: Real-Gas Effects and High Angles of Attack

    Prabhu, Dinesh K. / Papadopoulos, Periklis E. / Davies, Carol B. et al. | NTRS | 2005
    Keywords: Spacecraft Design, Testing And Performance

    The TPS Advanced Development Project for CEV

    Reuther, James / Wercinski, Paul / Venkatapathy, Ethiraj et al. | NTRS | 2006
    Keywords: Spacecraft Design, Testing And Performance

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