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Subset of X-57 Programmatic Summary Briefing
Space Environmental Exposure of the MISSE 9-15 Polymers and Composites Experiment 1-4 (PCE 1-4)
Aerodynamic and Acoustic Performance Testing of Metal Spacecraft Cabin Ventilation Fan
Realizing Rapid, Reduced-Cost High-Risk Research (R5)
Development of a deployable mechanism for a conical optical baffle for a small satellite
Stratospheric Test Methodology for Characterizing Free-Flight Dynamics of Entry Vehicles
A Guide to Forced Oscillation Data Processing and Analysis
Development of a dynamical model of a release mechanism for in-flight performance prediction
Lunar Safe Haven: Site Characterization and Preparation
Shock Tube Radiation Measurement in Expanding Air Flow
A Long-Lived Lander for Venus Surface Insitu Science
Relation between the Fatigue and Fracture Ductile-Brittle Transition in S500 Welded Steel Joints
Lunar Thermal Analysis Guidebook (L-TAG): Thermo-physical and Optical Properties of Lunar Regolith
RHU-RPS Long Duration Mars Hard Lander: Meteorology and Seismology Enabled by Radioisotopes (MASER)
Supersonic Transport Optimization to Mach 4
Marshall Space Flight Center Faculty Fellowship Program
Design and testing of a closing and sealing system for a Phobos sample return mission
MISSE-Flight Facility Polymers and Composites Experiment 1-4 (PCE 1-4)
Investigation of the in-flight anomalies of the LISA Pathfinder Test Mass release mechanism
Total Technical Life Extension Techniques for a Trainer Aircraft Airframe
Ceramic Insulated Slug Calorimeter for High- Enthalpy Flows
Flight Test of a Resistive Heating Coating for Visualizing Flow Transition
Passive Aeroelastic Tailored Wing Modal Test Using the Fixed Base Correction Method
Passive Aeroelastic Tailored Wing Modal Test Using the Fixed Base Correction Method
Resiliency, Reliability, and Sparing Approaches to Small Satellite Projects
Artemis Sustained Translational Acceleration Limits: Human Tolerance Evidence from Apollo to ISS
In-flight testing of the injection of the LISA Pathfinder test mass into a geodesic
Rocket Wake Flow Interaction Testing in the Hot Plume Testing Facility (HPTF) Cologne
The ‘FORESEE’ Prototype, Fully Active, Steered Two Axle Railway Vehicle
Solution of Maxwell’s Equations for Nonrectangular Electromagnetic Applications
Effect of Ram and Zenith Exposure on the Optical Properties of Polymers in Space
Companies Involved in Design, Manufacture, and Testing of Small Satellites
Small Satellites and Governmental Role in Development of New Technology, Services, and Markets
Kits, Components, and the Design, Manufacture, and Testing of Small Satellites
Small Satellites and Hosted Payloads for Technology Verification
Hosted Payload Packages as a Form of Small Satellite System
NASA's Space Launch System: Unmatched Volume for Deep Space Telescopes
Health Monitoring in Small Satellite Design