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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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NASA GRC PSL-3 Technical Challenges Full Scale Engine Test Facility Altitude and Sea Level Testing in an Ice Crystal Environment
No abstract available
Testing of a Liquid Oxygen/Liquid Methane Reaction Control Thruster in a New Altitude Rocket Engine Test Facility
No abstract available
Space Launch System Scale Model Acoustic Test Ignition Overpressure Testing
No abstract available
Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data
Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the NASA Langley National Transonic Facility, the NASA Ames 11-ft wind tunnel, and the European Transonic Wind Tunnel. In the NASA Ames 11-ft wind tunnel, data have been obtained at only a chord Reynolds number of 5 million for a wing/body/tail = 0 degree incidence configuration. Data have been obtained at chord Reynolds numbers of 5, 19.8 and 30 million for the same configuration in the National Transonic Facility and in the European Transonic Facility. Force and moment, surface pressure, wing bending and twist, and surface flow visualization data were obtained in all three facilities but only the force and moment and surface pressure data are presented herein.
Analysis of Load Test Annex (LTA) Floor Anchor Lateral Stiffness Test Results
No abstract available
Analysis of Load Test Annex (LTA) Floor Anchor Lateral Stiffness Test Results
No abstract available
SLS Flight Software Testing: Using a modified Agile Software Testing Approach
No abstract available
Integrated Cryogenic Propulsion Test Article and Thermal Vacuum Hotfire Test Results Overview
No abstract available
NASA Armstrong's Structural Dynamics Testing Capabilities and Testing Facility
No abstract available
ATD-1 Avionics Phase 2 Flight Test: Flight Test Operations and Saftey Report (FTOSR)
The Air Traffic Management Technology Demonstration-1 (ATD-1) is a major applied research and development activity of NASA's Airspace Operations and Safety Program (AOSP). The demonstration is the first of an envisioned series of Air Traffic Management (ATM) Technology Demonstration sub-projects that will demonstrate innovative NASA technologies that have attained a sufficient level of maturity to merit more in-depth research and evaluation at the system level in relevant environments.
Unmanned Aircraft Systems (UAS) Integration in the National Airspace System (NAS) Project Integrated Test and Evaluation Flight Testing Overview
No abstract available
Recent Radiation Test Results on a 22FDX Test Vehicle
Total ionizing dose irradiations were performed on a 22 nm fully-depleted silicon-on-insulator static random access memory. There is a strong well-bias effect in the TID response. Combined TID and SEE results are also presented.
Recent Radiation Test Results on a 22FDX Test Vehicle
Total ionizing dose irradiations were performed on a 22 nm fully-depleted silicon-on-insulator static random access memory. There is a strong well-bias effect in the TID response. Combined TID and SEE results are also presented.
Wear Test of the 12.5-kW Advanced Electric Propulsion System Engineering Test Unit Hall Thruster
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