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Search without synonyms: title: AIAA Scitech 2020 Forum

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    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 ...

    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 ...

    Mars Helicopter Technology Demonstrator

    Balaram, J. (Bob) / Canham, Timothy / Duncan, Courtney et al. | NTRS | 2018
    . Much like the Sojourner rover on the Pathfinder mission paved the way for the Spirit, Opportunity, Curiosity and the Mars 2020 rovers, an ...

    Reconstruction of the Advanced Supersonic Parachute Inflation Research Experiment Sounding Rocket Flight Tests with Strengthened Disk-Gap-Band Parachute

    Karlgaard, Christopher D. / Tynis, Jake A. / O'Farrell, Clara et al. | NTRS | 2019
    parachutes for future use at Mars. The flight tests are a risk-reduction program for the Mars 2020 mission. The flight tests involve two Disk-Gap ...

    Space Science and Technology Partnership Forum: Integration with Commercial In-Space Assembly Activities

    Benjamin, Gregory / Pensado, Alejandro / Arney, Dale C. et al. | NTRS | 2020
    The interagency Space Science and Technology (S&T) Partnership Forum was established in 2015 with participation from the United States Air ...

    Space Science and Technology Partnership Forum: Integration with Commercial In-Space Assembly Activities

    Benjamin, Gregory / Pensado, Alejandro / Mazarr, Alexander et al. | NTRS | 2020

    Flutter Analysis with Stabilized Finite Elements Based on the Linearized Frequency-Domain Approach

    Kevin E Jacobson / Bret K Stanford / Stephen L Wood et al. | NTRS | 2020

    Recent NASA Wind Tunnel Free-Flight Testing of a Multirotor Unmanned Aircraft System Vehicle

    John V Foster / Luke J Miller / Ronald C Busan et al. | NTRS | 2020

    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 ...

    Nonlinear Slosh Damping Testing and Analysis for Launch Vehicle Propellant Tanks

    Tannen S VanZwieten / Jacob M Brodnick / Shane Reese et al. | NTRS | 2020

    Nitric Oxide Laser-Induced Fluorescence Rotational Thermometry in a Hypersonic Non-Equilibrium Flow

    Connor C McDougall / Craig T Johansen / Roland Herrmann-Stanzel et al. | NTRS | 2020

    Subscale Demonstration and Validation of the Hercules Ascent, Descent, and Entry Vehicle

    Eytan Adler / Ethan Howell / Thomas McClure 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

    InSight Aerothermal Environment Assessment

    Beck, Robin A. S. / Songer, Jarvis T. / Szalai, Christine E. et al. | NTRS | 2020

    Development of a Thermal Management System for Electrified Aircraft

    Chapman, Jeffryes W. / Schnulo, Sydney L. / Nitzsche, Michael P. | NTRS | 2020