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Search without synonyms: title: AIAA Scitech 2020 Forum

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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

    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

    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 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 ...

    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 ...

    Computational Investigation of Powered Descent for Human-Scale Mars Landers

    Ashley M Korzun / Karen L Bibb / Francisco Canabal et al. | NTRS | 2020

    Computational Simulations of a Mach 0.745 Transonic Truss-Braced Wing Design

    Maldonado, Daniel / Housman, Jeffrey A. / Duensing, Jared C. et al. | NTRS | 2020

    Computational Simulations of a Mach 0.745 Transonic Truss-Braced Wing Design

    Maldonado, Daniel / Housman, Jeffrey A. / Duensing, Jared C. et al. | NTRS | 2020

    Computational Study of NASA's Quadrotor Urban Air Taxi Concept

    Ventura Diaz, Patricia / Yoon, Seokkwan | NTRS | 2020

    Control Force Compensation in Ground-Based Flight Simulators

    Chung, William W. / Zaal, Petrus M. T. / Terenzi, Lorenzo et al. | NTRS | 2020

    Control Force Compensation in Ground-Based Flight Simulators

    Chung, William / Zaal, Peter / Terenzi, Lorenzo et al. | NTRS | 2020

    Design of a Crossflow Attenuated Natural Laminar Flow Flight Test Article

    Michelle N. Lynde / Richard L. Campbell / Brett R. Hiller | NTRS
    scheduled to be completed at the end of 2019, with model fabrication beginning in early 2020.Design results presented in this abstract are ...

    Developmental Flight Instrumentation: Review of Space Shuttle, Ares I-X, and Artemis I

    Oleg O Goushcha | NTRS
    Center (HOSC). Following NASA's Artemis I Space Launch System (SLS) launch on November 16, 2020, data from three separate programs are available ...

    Developmental Flight Instrumentation: Review of Space Shuttle, Ares I-X, and Artemis I

    Oleg Goushcha | NTRS
    Center (HOSC). Following NASA's Artemis I Space Launch System (SLS) launch on November 16, 2020, data from three separate programs are available ...

    Development of a Thermal Management System for Electrified Aircraft

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

    Development of Unsteady Pressure-Sensitive Paint Application on NASA Space Launch System

    Roozeboom, Nettie H. / Powell, Jessie / Baerny, Jennifer K. et al. | NTRS | 2020

    Effects of Resistive Windscreens and Foam Inserts on The Acoustic Response of an In-Flow Phased Microphone Array

    W. Clifton Horne / Nathan J. Burnside / Stephen D. Schery et al. | NTRS | 2020

    FLEET Velocimetry in the Common Research Model’s Wing Wake

    Daniel T Reese / Paul M Danehy / Eric L Walker et al. | NTRS | 2020

    Fluid-Structure Interaction Simulations of the ASPIRE SR03 Supersonic Parachute Flight Test

    Francois Cadieux / Jordan B. Angel / Michael F. Barad et al. | NTRS
    parachute akin to the Mars 2020 mission that landed the Perseverance rover on Mars, and a higher freestream dynamic pressure prior to inflation. The ...

    Fluid-Structure Interaction Simulations of the ASPIRE SR03 Supersonic Parachute Flight Test

    Francois Cadieux / Jordan B. Angel / Michael F. Barad et al. | NTRS
    parachute akin to the Mars 2020 mission that landed the Perseverance rover on Mars, and a higher freestream dynamic pressure prior to inflation. The ...

    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

    Human-in-the-Loop Flight Simulation Experiment on Unmanned Aircraft Terminal Operations

    Devin Patrick Jack / Keith D Hoffler / Roy D Roper et al. | NTRS