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Challenges in Adjoint-Based Aerodynamic Design for Unsteady Flows
In-Situ Stress Measurement of Single and Multilayer Films for X-Ray Astronomy Optical Applications
Lunar Dust Characterization for Exploration Life Support Systems
Effect of Liquid Nitrogen Dilution on LOX Impact Sensitivity
Surface Profile Correction of Replicated X-Ray Optics Through Differential Deposition
High-Temperature Structural Instrumentation Developments for Hypersonic Airframe Applications
Effects of Contamination Upon the Performance of X-Ray Telescopes
X-Ray Optical Thin Film Deposition and Analysis Capability at NASA MSFC
James Webb Space Telescope (JWST): The First Light Machine
James Webb Space Telescope (JWST): The First Light Machine
Commercial Use of KSC's Cable Inspection Technologies and Potential Opportunities in the Near Future
The Insensitivity of Turbulent Flow to Changes in Reynolds Number and Mach Number
Laboratory Investigation of Countermeasures Receiving Set AN/ALR-2 (Xn-2)
Large Vehicle Portal Monitor for Perimeter Safeguards Applications
Navigator GPS Receiver for Fast Acquisition and Weak Signal Space Applications
The Use of Externally Mounted Preamplifiers in Antenna Arrays for the Meter Band
Mach Cutoff Analysis and Results from NASA's Farfield Investigation of No-Boom Thresholds
APOLLO Logistics Support Systems Molab Studies. TV Subsystem Studies for a Lunar Mobile Laboratory
OPTIMISM Experiment and Development of Space-Qualified Seismometers in France
Technical Considerations on Using the Large Nancay Radio Telescope for SETI
Economical Unsteady High-Fidelity Aerodynamics for Structural Optimization with a Flutter Constraint
James Webb Space Telescope (JWST) The First Light Machine
James Webb Space Telescope (JWST): The First Light Machine
Tropical Climate Variability During the Satellite Era: What Can We Infer About Climate Sensitivity
Sensitive Radar Search for Small Natural Satellites of the Earth
Qualification Tests of Active and Passive Dosimeters for APOLLO
Design of a Flush Airdata System (FADS) for the Hypersonic Air Launched Option (HALO) Vehicle
Piezoelectric Triaxial Accelerometer System for Use in Satellite Air Density Measurements
Microwave Landing System Accuracy Requirements for Automatic Flare-Out