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50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
Ablative Thermal Protection: An Overview
Ablative Thermal Protection Structure Design of Ballistic Reentry Spacecraft
ACEE (Aircraft Energy Efficiency) Composite Structures Technology
Acoustic Liner Feasibility Program Final Report, 19 Nov. 1968 - 19 Apr. 1970
Active Aeroelastic Tailoring of High-Aspect-Ratio Composite Wings
Activities of the Institute for Aerospace Studies of Toronto University
Activities Report of the French Aerospace and Research Industry
Adaptive Structures Flight Experiments
Additively Manufactured Lattice Structure Thermal Characterization
Aerospace Structural Potential of Beryllium, Dispersion Strengthened Metals, and Tantalum
A Lightweight 6 1/2-Ft Aeroshell for an Early MARS Probe Mission
Alpha Source Shaft Position Encoder Patent Application
A METHOD FOR PREDICTING THE PANEL FLUTTER FATIGUE LIFE OF SATURN 5 PANELS
Analysis of Alternate Hydrogen Sources for Lunar Manufacture
An Experimental Investigation of Panel Divergence at Subsonic Speeds
Anhysteretic and Remanence Curves of Metallic Recording Materials
Application of Electron and Laser Beams to Spacecraft Electronic Joining
A Review of the Status of Spacecraft Thermal Control Materials
Asteroid, Lunar and Planetary Regolith Management A Layered Engineering Defense
Atomic Oxygen Erosion of EVA-Stranded Soft-Goods on the ISS
Attenuation of Scattered Thermal Energy Atomic Oxygen
Attenuation of Scattered Thermal Energy Atomic Oxygen
Bacteriorhodopsin Films for Optical Signal Processing and Data Storage
Balloon Design for 9000 Pounds at 90,000 Feet: Recommendations Based on Heavy-Load Balloon History
Beryllium Fabrication Methods Development Program - Thermal Treatment
Carbon Fibre Reinforced Plastics - an Initial Evaluation
Catalogue of Reports and Reprints in World Data Center C Rockets and Satellites
Colloquium on Damage Mechanics of Graphite/Expoxy Laminates during Fatigue
Comparative Measurements of Earth and Martian Entry Environments in the NASA Langley HYMETS Facility
Comparative Method for the Evaluation of Array Reflector Materials
Contact Diffusion Interaction of Materials with Cladding
Continuation of NASA Rocket Motor Defects Investigation, June 1969 - May 1970
Controlled Atmosphere Sintering of Uranium Mononitride