Low-Pressure Plasma Cleaning of Aerospace Components Using Breathing/Compressed Air

A method for precision cleaning of aerospace components is needed that does not use hazardous or environmentally harmful commodities. Historically, precision cleaning methods have utilized solvents that have contributed to the depletion of the ozone layer or had high potential for contributing to global warming. Solvent cleaning produces large waste streams, and some solvents may be phased out in the future due to the environmental concerns.

Posted in: Briefs, Mechanical Components, Environmental technologies, Maintenance, Repair and Service Operations, Maintenance, repair, and service operations, Gases, Parts
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Chain Drive Dust Conveyer

The Mars 2020 coring drill will generate a significant amount of dust and debris (known as fines) due to the volume of milled material displaced by the corer's annulus. These cuttings must be removed to ensure that the drill does not jam. The typical method involves fluids, which may not work on Mars due to the atmospheric conditions.

Posted in: Briefs, Mechanical Components, Particulate matter (PM), Drilling, Mining vehicles and equipment, Spacecraft
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BiBlade Sampling Chain

The BiBlade sampler has been developed for potentially acquiring samples from the surface of a planetary body. The tool could conceivably be used in both in situ and notional sample return missions to planetary bodies including asteroids, comets, and moons. While the tool was designed for planetary sampling missions, it could have terrestrial applications as well.

Posted in: Briefs, Mechanical Components, Test equipment and instrumentation, Spacecraft
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Micro Acoustic Resonant Chambers for Heating/Agitating/Mixing (MARCHAM)

To measure organics in a fluid sample, one either has to bring the sample in the form of a colloid to the instrument, or extract the organics from the sample and bring the liquid extract to the instrument. The disclosed technique enables both extraction and transport of the fines or the organics.

Posted in: Briefs, Mechanical Components, Measurements, Acoustics, Acoustics, Test equipment and instrumentation
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Advanced Tool Drive System (ATDS) Camera Positioning Mechanism (CPM)

Robotic servicing of a satellite in low earth orbit (LEO) or geosynchronous Earth orbit (GEO) requires advanced systems capable of meeting the harsh environments of space. To support this effort, the Goddard Space Flight Center Satellite Servicing Capabilities Office (SSCO) has developed a camera positioning mechanism that will be capable of viewing features on a client satellite. Application of the CPM technology would be in multiple areas of spaceflight requiring robotic servicing including space exploration, planetary science, Earth science, and manned spaceflight.

Posted in: Briefs, Mechanical Components, Motion Control, Motors & Drives, Positioning Equipment, Optics, Optics, Maintenance, Repair and Service Operations, Maintenance, repair, and service operations, Robotics, Satellites
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Compact, Lightweight Trap Vent

This compact, lightweight trap vent is used to minimize the pressure differential of a high-altitude, balloon-borne detector. The vent allows the pressure to equalize rapidly, yet does not allow any light to enter the detector.

Posted in: Briefs, Mechanical Components, Gases, Exhaust valves, Test equipment and instrumentation
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Mechanical Actuators Bend as They “Breathe”

Extreme temperatures can severely strain a mechanical component because its material may have trouble enduring the heat without degrading. To address the problem, researchers at MIT developed a new material that expands and contracts as it lets oxygen in and out. The result is a new way to make actuators that could be used in extremely hot environments.

Posted in: INSIDER, Materials, Mechanical Components, Motion Control
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Robust, Highly Efficient Oxygen-Carbon Monoxide Cogeneration System

Oxygen, water, and fuel are of paramount importance to human life. As a leading concept, the solid-oxide electrolysis cell (SOEC) is a very powerful technology, especially in aiding NASA's endeavors to pursue extraterrestrial exploration missions. This work focused on developing a robust, long-life SOEC technology that efficiently cogenerates oxygen and CO fuel directly from CO2, and is superior to the state-of-the-art Oxygen-Generation System (OGS) technologies. The principal objective of the project was to develop the system to support Mars exploration missions as part of In-Situ Resource Utilization. The key problem characteristics were the SOEC performance and longevity under various operating conditions. The prior art was built on a thick electrolyte-supported SOEC using precious metals as electrodes. Due to the nature of SOEC operating mechanisms, high pressures may build up at the interfaces of the positive electrode and the electrolyte, resulting in electrode delamination and long-term stability issues. The state-of-the-art SOEC technology also faced the scaling up and stack sealing issues.

Posted in: Briefs, Mechanical Components, Carbon dioxide, Life support systems, Research and development, Oxygen
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Low Solidity Vaned Diffuser (LSVD) Design for Improvement of Pressure Recovery

Many pump vaned diffuser designs are based on existing airfoil designs, with little attention given to the vane leading edge. There is a need for a vaned diffuser leading edge that helps resist flow separation and the resultant poor diffuser pressure recovery. Diffusers in pumps are often working with an incompressible fluid that makes potential flow methodologies — which have incompressibility as a boundary condition — attractive. The potential flow-based free-streamline analysis methods have been known to improve the aerodynamics of varied components at high incidence angles, such as diffusers, jet engine nacelles, and liquid rocket engine turbopump inducers.

Posted in: Briefs, Mechanical Components, Airframes, Pumps, Aerodynamics
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Tangential Wrap Rib Deployable Reflector

There is a need for a large deployable reflector of 2-meter diameter or greater so smaller launch vehicles can be used. Common issues with going from a large solid reflector into deployable structures are the structural stiffness and deployable structure complexity.

Posted in: Briefs, Mechanical Components, Antennas, Antennas, Product development, Storage, Launch vehicles
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