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Optik
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Wireless Power Transfer Via Microwave for Mobilities
Optical Engineering and Educational Outreach at NASA
Using Optical Measurements to Characterize the Orbital Debris Environment in GEO
Marshall Space Flight Center’s X-ray and Cryogenic Facility
Early Results from NASA’s Laser Communications Relay Demonstration (LCRD) Experiment Program
NASA’s Mission: Exploring the Universe and Educating the Public
"NASA’s Mission: Exploring the Universe and Educating the Public
COUPLING INSTALLATIONS, STANDARD CONDUIT, ELECTRICAL
Capability Improvements at Marshall Space Flight Center's X-ray and Cryogenic Facility
Evaluation of OSAM-1 Camera Focus Shift in a Simulated Orbital Pressure Environment
HUBS, CONDUIT CONNECTION, STANDARD DIMENSIONS
Actuation System Data Summary for Missiles and Launch Vehicles
100BASE-T1 Un-Shielded Balanced Single Twisted Pair Ethernet Cable
A Study on Flexible Transparent Electrode Materials for Touch Sensor
Conduit, Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations
Connectors, Electrical, Reverse Bayonet, General Specification for
Electric Vehicle Power Transfer System Using Conductive Automated Connection Devices
Stationary Runway Weather Information System (In-Pavement)
Techniques for Suspect/Counterfeit EEE Parts Detection by Raman Spectroscopy Test Methods
MIL-PRF-29504/5, NSN 6060-01-6122316 Socket Terminus Alignment Sleeve Retention
Novel Laser Sources for Space-Based LIDAR and Communications Applications
Manufacturers’ Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories
Instrumentation for Impact Test—Part 2: Photographic Instrumentation
Current Status of NASA’s Low-Cost Optical Terminal (LCOT) at Goddard Space Flight Center
CABLE AND PLUG ASSEMBLY, EXTERNAL POWER 115/200 VOLTS 3 PHASE, SINGLE POINT REFUELING
Jet Characteristics of a Narrow Throat Pre-Chamber and Influence on the Main-Chamber Combustion
Visualization of Pre-Chamber Combustion and Main Chamber Jets with a Narrow Throat Pre-Chamber
High-Speed Thermographic Analysis of Diesel Injector Nozzle Tip Temperature
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC, JET STARTING
1000BASE-T1 Un-Shielded and Shielded Balanced Single Twisted Pair Ethernet Cable
A Guideline for Application of High-Density Fiber Optic Interconnects to Aerospace Platforms
Contacts, Electrical Connector, General Specification for
A Soiling Mitigation Method to Enhance the Performance of ADAS in Precipitation