Summary of radiation effects on thermionic insulator materials
Radiation effects on thermionic insulator materials - evaluation of beryllia, alumina, thoria, zirconia, and yttria
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Radiation effects on thermionic insulator materials - evaluation of beryllia, alumina, thoria, zirconia, and yttria
Fluorinated, chlorinated, and halogenated polymer adhesives prepared and tested for compatibility with liquid oxygen
Flow visualization and containment tests in directed-wall-jet vortex tube with radial outflow and moderate superimposed axial flows
Ligand containing polymers for use as heat sterilizable separators for silver zinc battery
Development, heat sterilization, and shock testing of silver-zinc cell
Mass spectroscopy and chemical deposition techniques for determining hydroxyl content in magnesium oxide
Portable spectrometer for monitoring oxygen and hydrogen as free gas or as dissociation products in inert gas shield of gas tungsten arc welding process
Communications, electronics, telemetry, command and control, and systems engineering for advanced space systems
Earth infrared horizon definition for space guidance, navigation, control, and pointing systems - feasibility study
Technical feasibility, costs, and benefits of using satellites in practical earth-oriented applications
This report summarizes the results of studies of economical orbital transportation systems, exploring, in particular , possible options for time - phases and incremental development of such systems. The major conclusions are : 1. Incremental development is a practical way for development of an economic logistics system, minimizing development risk and annual funding, and offering planning flexibility at only a nominal penalty in total systems cost. 2. The most promising first development appears to be that of a re- usable payload carrier with a capacity of 9 to 12 passengers. 3. Systems comparisons show that, for the foreseeable variations of the mission market, a partially reusable concept could bring about most of the program savings that can be expected from reusability at moderate development risk and funding rate. 4. A further development leading to a fully reusable system has high risk and uncertain payoff. Conceivably, at that time, a more advanced concept might be introduced.
Performance tests of short length, gas turbine combustors with atomized or vaporized fuel injection
Rolling disks for evaluation of high speed, high temperature lubricant applications
Degradation of radiator surfaces due to lunar dust contamination and removal/prevention concepts
Systems engineering update of preliminary spacecraft configuration for Voyager 1973 mission
Atlas Agena Applications Technology Satellite-C mission, launch operations plan, communications, and prelaunch tests
Beam alignment techniques developed for infrared sensitive single crystal germanium to study multiplication effect in photoconductors
Systems engineering data and recommended Voyager spacecraft configuration for Martian launch opportunities - 1973-1979