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    Adaptive Hexapod Simulator Motion Based on Aircraft Stability

    Zaal, Peter M. T. / Popovici, Alexandru / Lewis, Emily K. | NTRS | 2020

    Advances in Low-Cost Manufacturing and Folding of Solar Sail Membrane

    Olive R Stohlman / Juan M Fernandez / Gregory D Dean et al. | NTRS

    Aeroheating Measurements of BOLT Aerodynamic Fairings and Transition Module

    Rieken, Elizabeth F. / Berry, Scott A. / Broslawski, Casey J. et al. | NTRS | 2020

    Airborne Science Mission Capabilities of the NASA DC-8 and Possible Alternative Aircraft

    Thomas A Ozoroski / James W Fenbert / Nicholas K Borer et al. | NTRS | 2020

    An Overview of NASA’s Learn-to-Fly Technology Development

    Stephen E Riddick | NTRS | 2020

    A Numerical Investigation of Parachute Deployment in Supersonic Flow

    Boustani, Jonathan / Anugrah, Gokul / Barad, Michael F. et al. | NTRS | 2020

    A Numerical Investigation of Parachute Deployment in Supersonic Flow

    Boustani, Jonathan / Anugrah, Gokul / Barad, Michael F. et al. | NTRS | 2020

    Application of Risk Informed Decision Making to a Highly Reliable Three-Dimensionally Woven Thermal Protection System for Mars Sample Return

    Needels, J. / Gage, P. / Ellerby, D. et al. | NTRS | 2020

    Application of Risk Informed Decision Making to Highly Reliable Three Dimensionally Woven Thermal Protection System for Mars Sample Return

    Needels, J. / Gage, P. / Ellerby, D. et al. | NTRS | 2020

    Artificial Thickening of a Transonic Boundary Layer in the Presence of a Pressure Gradient Associated with a Boundary Layer Ingestion Concept

    Gregory S Jones / William Milholen / Alaa Elmiligui et al. | NTRS | 2020

    A Simulation Framework for Precision Landing and Hazard Avoidance Technology Assessments

    Alicia Dwyer Cianciolo / Soumyo Dutta / Rafael Lugo et al. | NTRS | 2020

    ASPIRE Parachute Modeling and Comparison to Post-Flight Reconstruction

    Soumyo Dutta | NTRS | 2020
    2020 mission parachute. Prior to all three flights, a multi-body flight dynamics simulation was developed to predict the parachute dynamics and ...

    Assessment of Mars 2020 Forebody Heating Predictions with Coupled Material Response

    Tom West / Chris Johnston | NTRS

    Assessment of the Mars 2020 Entry, Descent, and Landing Simulation

    David W Way / Soumyo Dutta / Carlie H Zumwalt et al. | NTRS
    On February 18, 2021, the Mars 2020 Perseverance rover successfully landed inside Jezero Crater at 18.44463 deg North latitude and 77.45088 ...

    Assessment of the Performance Potential of Advanced Subsonic Transport Concepts for NASA's Environmentally Responsible Aviation Project

    Nickol, Craig L. / Haller, William J. | NTRS | 2016
    ) of 4-6 by 2020. Progress towards this fuel burn reduction target was measured through the conceptual design and analysis of advanced subsonic ...

    Assessment of Transition Modeling Capability in OVERFLOW with Emphasis on Swept-Wing Configurations

    Balaji Shankar Venkatachari / Pedro Paredes / Joseph M Derlaga et al. | NTRS | 2020
    wing introduced by the Technical University of Braunschweig, and the wing-body configuration of the CRM model from the fourth and fifth AIAA ...

    Autonomous Real-Time Global Aerodynamic Modeling in the Frequency Domain

    Eugene A Morelli | NTRS | 2020

    Benefit Assessment of the Integrated Demand Management Concept for Multiple New York Metroplex Airports

    Yoo, Hyo-Sang / Evans, Antony D. / Kulkarni, Deepak et al. | NTRS | 2020

    Building Maps for Terrain Relative Navigation Using Blender: An Open-Source Approach

    Kyle W Smith / Nicholas Anastas / Andrew S Olguin et al. | NTRS
    validated by reproducing imagery collected during a flight of New Shepard in October 2020 and was further used to generate reference maps for use by ...

    Capability and Technology Performance Goals for the Next Step in Affordable Human Exploration of Space

    Linne, Diane L. / Sanders, Gerald B. / Taminger, Karen M. | NTRS | 2015
    to be flown on the Mars 2020 robotic lander is in development. However, many of the individual components still require technical ...

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