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X-57 Mod II Avionics Power Analysis
The Value of "Test-As-You-Fly": Modernizing Experimentation and Data Analysis for NASA Missions
Space Launch System: Sensor Analysis, Modeling, and Test for Robust Propulsion System Autonomy
A Common Probe Design for Multiple Planetary Destinations
Sensor Arrays for Aerospace Vehicles
Orion Powered Flight Guidance Burn Options for Near Term Exploration
Steering of Solar Sails Using Optical Lift Force
System Engineering Principles of Complexity
Capture Latch Assembly for the NASA Docking System
NASA's Space Launch System Status
X-57 Cruise Motor and High-Lift Motor Mission Profile Power Analysis
HAT Tricks: Understanding Human Autonomy Teaming Through Applications
NASA LaRC Full Scale F28 Barrel Drop Summary: With Analysis Suited for ARAC TACDWG
Surveys of Returned ISS Hardware for MMOD Impacts
ATM-X X3 Simulations Boeing Briefing May 20th, 2020
Astrobee Overview: System, Status, Performance, and Specification
ADEPT Sounding Rocket One Flight Test Overview
Space Launch System Mobile Launcher Modal Pretest Analysis
Design of a Microgravity Hybrid Inflatable Airlock
NASA-SSC Rocket Plume Deflector Testing and Analyses
Space Launch System: SLS Payload Delivery Capability Overview
Studies in Support of Venus Aerocapture Utilizing Drag Modulation
Ground System Spares/Maintenance Plans Derived from Limited Life Item Analysis
LA-8 Conceptual Design Model Release to OpenVSP Hangar
NASA WG3 MMOD Protection Summary
Advanced Aeromechanics Prediction Methods for Rotorcraft Flight Vehicles
Temporal Evolution of the Plasma Sheath Surrounding Solar Cells in Low Earth Orbit
Temporal Evolution of the Plasma Sheath Surrounding Solar Cells in Low Earth Orbit
Human Mars Ascent Vehicle Configuration and Performance Sensitivities
Mars Ascent Vehicle Sizing, Habitability, and Commonality in NASA's Evolvable Mars Campaign
Low Temperature Electrolytes in High Specific Energy 18650 Li-Ion Cells for Future NASA Missions
Radio Occultation Retrieval Using Phase Matching and Optimization
HyTES Recent Campaigns and Transition to High Altitude Platform
Small Spacecraft Technology Program
JPL Minimum Mars Architecture Notional Vehicle Configurations
Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters
You Want to Fly What Kind of Hardware?