Physical Sciences

Physical Causes of Extremely Low Geomagnetic Activity

NASA’s Jet Propulsion Laboratory, Pasadena, California

An analysis of solar, solar wind, and geomagnetic data during the recent solar cycle minimum (2008) has recently been undertaken. It was discovered that the lowest value of the Ap index [this index is an averaged planetary A index based on data from a set of specific magnetometer stations] in the history of its recording occurred during 2009, about 1 year after solar minimum. The investigators were able to determine that it was the decrease of solar and interplanetary forcing that was causing the anomalous effect. The coronal holes, which emit high-speed solar wind plasma streams, were located at middle (solar) latitudes during this epoch of the solar cycle. Thus the full brunt of the solar wind and its embedded Alfvén waves missed the Earth and its magnetosphere, lessening the effect of the solar wind-magnetosphere interaction.

Posted in: Briefs, Physical Sciences, Analysis methodologies, Data acquisition, Data acquisition (obsolete), Test procedures, Satellites

Green PCB Removal From Sediment Systems (GPRSS)

A redeployable polymer blanket attacks and adsorbs PCBs.

John F. Kennedy Space Center, Florida A number of NASA centers have used polychlorinated biphenyl (PCB)-containing materials that have subsequently ended up in surrounding sediment systems. Each center is evaluating remediation technologies that may have application to their environmental problems; however, there are only limited options available for application to sediments containing PCBs. Currently, the most utilized option is dredging followed by disposal in a Toxic Substances Control Act (TSCA)-regulated landfill. This is an expensive option with long-term liability implications for simply enacting a waste transfer remedy (as opposed to a waste destruction alternative), as well as possible contaminant re-introduction into the water table. PCB contamination in sediment systems is a global issue, posing ecological and human health risks.

Posted in: Briefs, Physical Sciences, Ethanol, Medical, health, and wellness, Waste disposal, Magnesium, Polymers, Hazardous materials

Internalization of Non-Spherical Particles

This device enhances proliferation of cell cultures in a rotating bioreactor.

This invention specifically relates to an interchangeable sleeve that encompasses a rotating, substantially cylindrical bioreactor. The sleeve supplies a time-varying electromagnetic force of from 0.05 to 0.5 gauss to the culture chamber of the bioreactor in order to increase cell growth and proliferation within the rotating bioreactor. The sleeve comprises a substantially cylindrical and rigid, electrically conductive material wound in a cylindrical shape, and is capable of being connected to a pulsating, time-varying electromagnetic current.

Posted in: Briefs, Physical Sciences, Electromagnetic compatibility, Medical, health, and wellness

System for Observing Dynamic Atmospheric Phenomena

System has drastically increased transmitter capability at much reduced cost.

NASA’s Jet Propulsion Laboratory, Pasadena, California

Existing observing systems are inadequate to measure a variety of dynamic atmospheric processes. Ground-based or airborne systems do not observe over sufficiently large regions to capture the context or time history of many phenomena. Space-based systems do not observe a specific region over sufficient duration with sufficient spatial resolution to capture the essential features of the phenomena. Radar systems are limited in what they can observe because of the need for scattering sources to be present in the observed volume.

Posted in: Briefs, Physical Sciences, Antennas, Data acquisition, Data acquisition (obsolete), Test equipment and instrumentation, Satellites

Covariance Analysis of Astrometric Alignment Estimation Architectures for Precision Dual-Spacecraft Formation Flying

A paper highlights analysis of proposed navigation systems and architectures for achieving precise dual-spacecraft astrometric alignment. The dynamics of dual-spacecraft relative motion, within a restricted n-body problem framework, are shown to reduce to a simple linear form for use in estimation filter design and error analysis for a deep space mission application, such as MASSIM (Milli-Arc-Second Structure Imager). This model is augmented with simplified measurement process models of relevant measurement types. These include inertial sensors, such as accelerometers and rate gyros, as well as optical alignment sensors, such as star and laser beacon trackers. A consider-state covariance analysis tool is developed from these process models and used to study the performance of proposed estimation architectures for the MASSIM application. This work develops a generic analysis methodology for evaluation of dual-spacecraft relative navigation systems and architectures for precise dual-spacecraft astrometric alignment.

Posted in: Briefs, TSP, Physical Sciences, Mathematical models, Architecture, Sensors and actuators, Spacecraft guidance

Automated Purgatoid Identification

An algorithm was developed that automatically processes images captured by the HiRISE camera on the Mars Reconnaissance Orbiter to identify and locate the presence of purgatoids in monochrome images.

Posted in: Briefs, TSP, Physical Sciences, Mathematical analysis, Computer software and hardware, Imaging and visualization, Identification, Satellites

Interplanetary CubeSats

A report describes upgraded CubeSat satellite elements for the interplanetary environment, with solar sail propulsion and the interplanetary superhighway for navigation and maneuvering. They can host small, capable instruments and optical telecommunications on a mission to map the composition of a sequence of near-Earth asteroids and planetary bodies.

Posted in: Briefs, TSP, Physical Sciences, Imaging and visualization, Satellite communications, Solar rocket engines, Test equipment and instrumentation, Satellites

Spacecraft Line-of- Sight Stabilization Using LWIR Earth Signature

Applications could include remote science and planetary science missions, Earth surveillance and reconnaissance, and deep space optical communication.

Until the time of this reporting, when a space vehicle required a reference signal for inertial pointing, the choices were a signal beacon from an Earth location, the Earth radiance in the visible spectrum, or a star tracker. However, limitations can arise from using these techniques. For example, the signal beacon suffers from limited signal power (either in RF or optical) and will constrain the application to limited ranges, errors due to stray-light and centroiding limit the accuracy of a star tracker, and the spatial/temporal variability of the Earth’s albedo and its illumination by the Sun introduces limitations when used in the visible or near infrared light.

Posted in: Briefs, Physical Sciences, Spacecraft guidance

Transportable Instrumentation Package for In-Vehicle On-Road Data Acquisition

This portable data acquisition system is a viable alternative to first developing a fully instrumented test vehicle.

The study of driver behavior can provide a wealth of information that can be useful in the design of automobiles including active safety features and functions. There may be differences in driver behavior, as reflected in driver state, and these differences may be confounded by a driver’s condition. Much can be learned from studies that look at driver state and condition to answer questions such as how vehicle features and functionality could be designed to complement the driver’s capabilities and limitations in the vehicle. Also, a better understanding could be gained to determine how, or if at all, a safety feature’s characteristics should be modified to accommodate a driver’s condition.

Posted in: Briefs, Physical Sciences, Data Acquisition, Human factors, Data acquisition, Data acquisition (obsolete), Test equipment and instrumentation

Variable Camber Aerodynamic Control Surfaces and Active Wing Shaping Control

Concepts are examined to reduce aerodynamic drag and decrease fuel consumption.

A new concept of aircraft aerodynamic control surfaces has been developed in connection with another new concept of active wing shaping control for reducing aircraft drag that will result in less fuel burn. The first concept is referred to as a variable camber continuous trailing edge flap or, alternatively, a variable camber continuous leading edge slat. The variable camber trailing edge flap (or leading edge slat) comprises multiple chord-wise segments (three or more) to form a cambered flap surface, and multiple span-wise segments to form a continuous trailing edge (or leading edge) curve with no gaps that could be prescribed by a mathematical function or the equivalent with boundary conditions enforced at the end points to minimize tip vorticities. Aerodynamic simulations have shown that this type of flap can reduce aerodynamic drag substantially as compared to a conventional flap. A new active wing-shaping control concept is proposed in connection with the presently disclosed variable camber continuous trailing edge flap (or leading edge slat). The active wing-shaping control is designed to change a wing shape in-flight in order to achieve a desired optimal wing shape for optimal drag reduction.

Posted in: Briefs, Physical Sciences, Wings, Aerodynamics, Aircraft

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