Infra-Red and Electro-Optics. Test and Evaluation of an Ultraviolet Objective Spectrograph
Ultraviolet objective spectrograph for hand operation by mercury astronaut
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Ultraviolet objective spectrograph for hand operation by mercury astronaut
RJ-1 fuel surface potential is measured with a probe to determine the degree of hazard originating from static electricity buildup in the hydraulic fluid. The probe is mounted in contact with the fluid surface and connected to an electrostatic voltmeter.
Three separate mechanisms test the insulation on electrical wire specimens for mechanical resistance to flexure, abrasion or wear, and vibration. The test mechanisms perform the evaluation tests on insulated wire specimens in a chamber which can be controlled to simulate space or spacecraft cabin environments.
Polymeric materials in expulsion bladders for cryogenic liquids, describing fabrication, flexibility, permeability, storage, transfer, control factors, etc
Cathodic catalysts evaluated for hydrazine-air fuel cells employing alkaline electrolytes
Ground facilities for determining structural characteristics, performance capabilities, and reliability of rockets in space environments
Material selection, and design and evaluation of hybrid nozzles for operation in FLOX lithium base propellant environment
Corrosion resistance and anode activity data on interstitial compounds for fuel cell catalysts
Equipment requirements for checkout of missiles, space vehicles and spacecraft to establish performance during mission life, discussing control and problem solving
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Anode configurations for xenon lamps
Injector compatibility improvement for Apollo lunar module descent engine ablative chamber
Radiation effects on performance of thin film pressure transducers
Assessment of molded elastomeric Teflon as seat seal material for R4D engine valve
Neutron flux distribution in water for strong Am- Be neutron source enclosed in Be spheres, comparing calculated and measured flux distributions
Flight and control specimens 6, 9, and 12 from the Apollo 14 composite casting demonstration were evaluated with respect to the degree of dispersion achieved for mixtures of immiscible materials under one-gravity and low gravity environments. The flight and control capsules 6, 9, and 12 contained paraffin and sodium acetate; paraffin, sodium acetate and argon; and paraffin, sodium acetate and 100 micrometer diameter tungsten microspheres, respectively. The evaluation and documentation utilized photographic and microstructure examinations, density measurements, and droplet size and distribution determinations. In addition, theoretical analyses were performed in order to aid in the understanding of the fluid behavior of the specimens during processing and subsequent solidification. A comparison of evaluated data with the theoretical analyses reveals that although the immiscible materials were uniquely dispersed in a low gravity environment, nonuniform dispersions were obtained primarily due to insufficient initial mixing and an essentially unidirectional thermal gradient during cooldown.
The results of experiments 1, 2, and 10 of the Apollo 14 composite casting demonstration are discussed. The purpose of the demonstration, with regard to samples 1 and 2, was to obtain preliminary data on the liquid phase sintering process in a weightless environment. With regard to sample 10, the purpose was to obtain preliminary information on how to achieve uniform dispersion of dense particles on a metal matrix by employing shaking modes or forces in the system when the metal matrix is molten. Results of the demonstrations were interpreted in a quantitative and qualitative manner. For experiment 1 it was found that the tungsten particles were redistributed more uniformly in the flight sample than in the control sample. Experiment 2 results indicate that complete melting may not have occured and thus a high degree of significance cannot be associated with the qualitative results relating to particle redistribution data. The particle-matrix system of experiment 10 was found to be nonwetting.