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Lunar Safe Haven: Site Characterization and Preparation
ISVAR: In-Situ Validation of Augmented Reality
Shock Tube Radiation Measurement in Expanding Air Flow
X-57 Mod II Avionics Power Analysis
The Value of "Test-As-You-Fly": Modernizing Experimentation and Data Analysis for NASA Missions
Design of an Open Rotor, Braced-Wing Electric Transport
NASA TECHNICAL STANDARD, NASA-STD-7012A, LEAK TEST REQUIREMENTS
Rapid Flight Control Law Deployment and Testing Framework for Subscale VTOL Aircraft
ROSA and Solar Cell Module Combined Environments Test Plan
Propulsive Descent Technologies - Powered Descent Retropropulsion in an Atmosphere
Gateway Utilization Capabilities and Status
Closing of Critical Technology Gaps for High-Efficiency Rotating Detonation Rocket Engines
Regenerative Exploration ECLSS Technology Development
Blue Origin De-orbit Descent and Landing Tipping Point: Program Final Report
Design, Control, and Simulation of Tensegrity Based Kites
Mars Ascent Vehicle: Presentation to Powell County High School
Simulated Excavation Environment for Lunar Operations
A Long-Lived Lander for Venus Surface Insitu Science
A Rideshare Tensegrity Rover Concept to Explore Titan’s Lands and Oceans
Lunar Transport Vehicle Occupant Protection Requirements
Implementation Approach for an Electrified Aircraft Concept Vehicle in a Research Flight Simulator
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)
RHU-RPS Long Duration Mars Hard Lander: Meteorology and Seismology Enabled by Radioisotopes (MASER)
NASA’s Strategic Analysis Cycle 2021 (SAC21) Human Mars Architecture
Power System Design Trades for a Pressurized Lunar/Mars Rover
Development and Sizing of the Mars 2020 Thermal Protection System
Development and Sizing of the Mars 2020 Thermal Protection System
An Overview of Spacecraft Design for Piloting, Manual Control, and Handling Qualities
Mars Entry Instrumentation Flight Data and Mars 2020 Entry Environments
Full Life Cycle Mach 6 Nozzle Testing at Long Duration
Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft
Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft
Aero-Propulsive Modeling for eVTOL Aircraft Using Wind Tunnel Testing with Multisine Inputs
Technology Readiness Level (TRL) as the foundation of Human Readiness Level (HRL)
SLS-SPEC-159, Cross-Program Design Specification for Natural Environments (DSNE)
Total Technology Readiness Level: Accelerating Technology Readiness for Aircraft Design
Space Shuttle Cargo Integration Coupled Loads Analysis Lessons Learned
Scalable Autonomously Configured Integrated DAQ/Control System
Feasibility Analysis of Unmanned Aerial Vehicle Based on Tensegrity Structure
Supersonic Transport Optimization to Mach 4
The Causes of Propeller Pitching Moment and the Conditions for its Significance
Projects at NASA: Factors Driving Mission Success