Cryogenic high-speed transmitter and receiver circuits in advanced CMOS technology for quantum computing and technology
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Since its establishment, the Heliostat Consortium (HelioCon) has made substantial progress toward closing many of the gaps in concentrating solar power (CSP) research. Numerous techno-economic studies have been performed, investigating topics ranging from the trade-off between size and temperature for industrial process heat applications to optimization of the heliostat design itself for various applications. Significant improvements have been made in optical metrology techniques, with first steps toward in situ measurement of heliostat fields. Several standards have been, and continue to be, developed with the coordination of an international group of CSP industry participants. Training programs have been developed, with universities including CSP in their engineering curricula, and many public webinars have been held to provide broad access to the latest CSP research. Improved CSP components such as mirror facets and wireless communication systems have been developed, and the solar tower at Sandia National Laboratories has been upgraded with a testbed for closed-loop controls research and development. Field deployment challenges involving heliostat foundations and sensitive wildlife habitats have been explored, with progress made toward methods for streamlining project development and permitting. Additional knowledge has been added to the body of work on wind behavior of heliostats and arrays of heliostats, with progress made toward a holistic understanding of wind design methods. Finally, techniques have been developed and demonstrated for assessing soiling conditions at a proposed project site, with predictive models for the soiling rate showing good results. Taking these results together, HelioCon has contributed greatly to the global CSP research and development effort over the past several years.
Fundamentals of friction and wear on fluid film and rolling-element bearings
Valve technology for spacecraft and rocket engine applications, discussing zero-gravity vent valve, zero leakage valve, insensitive valve seat and solenoid actuator
Structural technologies applicable to future large launch vehicles
Voltage breakdown phenomena - high voltage packaging techniques and test equipment
Gas impermeable and cryogenic flexible protein films
Part control package using long-life transistor as example for ultrahigh-reliability inspection in advanced planetary missions
Proposed contractual requirements to implement ultrahigh-reliability of parts for advanced planetary missions
Transistor, resistor, capacitor, diode, and integrated circuit used as examples of ultrahigh reliability appraisal in advanced planetary missions
Problem areas within cryogenic chemical and nuclear propulsion systems for space missions, noting available technology and limitations
Application of electronic technology to design and development of integrated circuit, telemetry system for biomedicine
Development and characteristics of elastomeric materials for positive expulsion bladders
Engine and stage design criteria on sizing requirements of complete stage for LOX/hydrogen engine
Regenerative cooling system design for rocket engines
Research conducted during this period is reported. Studies presented include: (1) diffusion and permeation of CO2, O2, N2, and NO2 through polytetra fluoroethylene; (2) diffusion, permeation and solubility of simple gases (CO2, O2, N2, CH4, C2H6, C3H8, and C2H4) through a copolymer of hexafluoro propylene and tetrafluoro ethylene (FEP); (3) viscous flow and diffusion of gases throug small apertures; (4) diffusion and permeation of O2, N2, CO2, CH4, C2H6, and C3H8 through nitroso rubber; and (5) results of gas transport studies with carborane siloxane, nitroso rubber, silicone membrane, krytox coating on teflon, and FEP coated glass cloth. Publications generated under this program are listed.
Investigations are presented concerning design concepts and implementation approaches for the satellite communication repeater subsystems of advanced multifunctional satellites. In such systems the important concepts are the use of multiple antenna beams, repeater switching (routing), and efficient spectrum utilization through frequency reuse. An information base on these techniques was developed and tradeoff analyses were made of repeater design concepts, with the work design taken in a broad sense to include modulation beam coverage patterns. There were five major areas of study: requirements analysis and processing; study of interbeam interference in multibeam systems; characterization of multiple-beam switching repeaters; estimation of repeater weight and power for a number of alternatives; and tradeoff analyses based on these weight and power data.