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Loads and Structural Dynamics Requirements for Spaceflight Hardware
Radiant Heater Test Facility (RHTF) NASA Johnson Space Center
Subset of X-57 Programmatic Summary Briefing
Historical Retrospective on Orion GNC Design
Wheel Module Motor Trade Study for Lunar Terrain Vehicle Thermal Control System
A Distributed Simulation Framework Applied to Artemis Analysis, Studies, Integration, and Test
Design of a Family of Mars Chemical Transportation Elements
Johnson Space Center Thermal Technology Roadmap 2024
In Situ Sensors for Monitoring the Space Environment and Its Effect Upon Satellite Materials
X-57 Mod IV Avionics Power Analysis
Dragonfly Entry and Descent Overview
Realizing Rapid, Reduced-Cost High-Risk Research (R5)
Effects of Ambient Conditions on Helicopter Harmonic Noise Radiation: Theory and Experiment
Preparing for Exploration from the Surface of Our Sister Planet
Lessons Learned from Large-Scale Aerospace Structural Testing
Transient Liquefaction on the Lunar or Martian Surface Operational Demonstration
Particle Seeding System Upgrades in the NASA GRC 1 × 1 Supersonic Wind Tunnel
Structural Design and Aeromechanical Analysis of Unconventional Blades for Future Mars Rotorcraft
Advances in Aircraft System Identification at NASA Langley Research Center
Desert Research and Technology Studies (D-RATS) 2022 Test Report
Computer Human Interface Challenges in Space Exploration
X-57 Mod II Avionics Power Analysis
The Value of "Test-As-You-Fly": Modernizing Experimentation and Data Analysis for NASA Missions
NASA TECHNICAL STANDARD, NASA-STD-7012A, LEAK TEST REQUIREMENTS
Mars Ascent Vehicle: Presentation to Powell County High School
Simulated Excavation Environment for Lunar Operations
Lunar Thermal Analysis Guidebook (L-TAG): Thermo-physical and Optical Properties of Lunar Regolith
Lunar Thermal Analysis Guidebook (L-TAG)
Lunar Thermal Analysis Guidebook (L-TAG)
An Overview of Spacecraft Design for Piloting, Manual Control, and Handling Qualities
SLS-SPEC-159, Cross-Program Design Specification for Natural Environments (DSNE)
Projects at NASA: Factors Driving Mission Success
X-57 Cruise Motor and High-Lift Motor Mission Profile Power Analysis
Scalable Autonomously Configured Integrated DAQ/Control System
Unsteady Propagation and Mean Corrections in Open-Jet and Kevlar® Wind Tunnels