Effect of solid propellant rocket exhaust impingement on spacecraft materials Final report, 18 Mar. 1966 - 21 Feb. 1969
Solid propellant rocket exhaust impingement effect on spacecraft materials
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Solid propellant rocket exhaust impingement effect on spacecraft materials
Vapor deposition of single crystal thin films of lithium ferrite utilizing ferric chloride
Damage structure due to 1 to 5 MeV electron irradiation studied in lithium diffused silicon for solar cells
High temperature LM cathode ion thrustors
Vacuum deposition parameters for titanium-silver contacts on silicon solar cells
Integral cover-glass coatings applied to silicon solar cells by radio frequency sputtering for radiation and thermal protection
Permeability characteristics of membranes
Data analysis of GEOS 1 tracking network
Botanical systems tested for effects by lunar soil
Theory and design of small scale lunar surface personnel transporter using hopping mode
Development of silicon carbide hot electron emitter
Sintering of INCO and carbonyl nickel powder for preparing plaques for use in nickel cadmium batteries
Long range planning for solar system exploration
Accelerating plasma diagnostics - validity of local thermal equilibrium assumption in electromagnetic shock tubes, and current-sheet velocity in coaxial plasma accelerator
High temperature breakdown of cesium vapor through insulating material cracks
Structure of radiation damage in lithium diffused solar cells
Design improvements in silver-zinc battery for space application
Reliable techniques for making electrodes from powders of gold chloride and aluminum