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    NASA University Research Centers Present a

    Virtual Poster Session and SymposiumWelcome to the NASA University Research Centers (URC) Virtual Poster Session and Symposium(VPSS). This is a unique opportunity to meet NASA URC students and learn about their exciting

    experiences as summer 2012 interns or co-ops at NASA centers.

    Browse the poster presentations below to see a description and visual representation of researchprojects that URC students completed under the guidance of NASA mentors.

    You can leave questions or comments for student presenters using accounts on Facebook, Yahoo,Hotmail and AOL. The comment section is at the bottom of each project page.

    URC students welcome your feedback during the VPSS. If you are a poster session judge, students

    will respond to you within 24 hours of your post.

    To learn more about the NASA URC Program,

    Please visit us at the following websites:

    http://www.nasa.gov/offices/education/programs/national/urc/home/index.html

    http://www.facebook,com/NASAURC1

    http://www.nasa.gov/offices/education/programs/national/urc/home/index.htmlhttp://www.facebook%2Ccom/NASAURC1http://www.facebook%2Ccom/NASAURC1http://www.nasa.gov/offices/education/programs/national/urc/home/index.html
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    Virtual Poster Sessionand Symposium

    2012 Summer Intern ParticipantsPage

    Raul Acevedo 3

    Adeyemi Adegbite 4

    Juan M. Barragan 5

    Billy Barrios 6

    Tara Blakey 7

    Harry Burton III 8

    Kalind Carpenter 9

    Stanford Carter 10Frank Ceballos 11

    Vanessa Dorado 12

    Robert Ellis 13

    Jordan Fuchs 14

    Raul Garcia-Sanchez 15

    Zenia Garcia 16

    Valeria C. Arce Gonzalez 17

    Kelly Courtney Gustafson 18

    This VPSS is open to the NASA URC community and the public.

    The competition and judging portion of the poster session will

    run from Oct. 24- 31, 2012.

    Winners and runners-up in the three categories listed below will

    be announced on Nov. 1, 2012. These individuals will be invited

    to give an oral presentation of their research to the NASA URC

    community at a Virtual Symposium on Nov. 8, 2012.

    For additional details, contact the NASA URC Management Office

    via [email protected] [email protected].

    Poster Categories: Aeronautics Research (ARMD)

    Human Exploration and Operations (HEOMD)

    Science (SMD)

    PageDaniel H. Hernandez, Jr. 19

    Jesus Hinojosa 20

    Adrienne Lam 21

    Alberto Mata 22

    Jose A. McKinnon 23

    Hctor Mendez-Colberg 24

    Kevin J. Monk II 25

    Gregory Morales 26Brandon Norman 27

    Ryan OConnor 28

    Edwin Ortiz-Quiles 29

    Francisco Pena 30

    Darian Phillips 31

    Zachary Roberts 32

    Rigoberto Roche 33

    Robert Conrad Rorie 34

    Janet Ruedas 35

    Kimberlin Schnittaker 36

    Christopher St. Julian 37

    Eric Thomas 38

    Loraine Torres-Castro 39

    Viviana Villamizar 40

    Michael Joseph Williams 41Jason Ziccardi 42

    mailto:[email protected]:[email protected]:[email protected]:[email protected]:[email protected]:[email protected]
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    Raul AcevedoUniversity of Puerto Rico, Rio PiedrasMajor: Chemical Physics

    Degree Level: Ph.D.

    Intern Site: NASA Kennedy Space Center

    Mentor: Dr. Luz M. Calle

    Electrokinetic deposition of methylmethacrylate is used to mitigate

    corrosion in reinforced concrete. The methylmethacrylate (MMA)

    monomer deposits in the pores in the concrete where it is converted into

    its polymer, polymethylmethacrylate, thus creating a barrier that also

    enhances the mechanical properties of the concrete. Previous to the MMA

    treatment, an electrokinetic deposition is used to transport calcium,

    sodium and potassium hydroxide particles through the capillary pores of

    concrete directly to the concrete reinforcement. The intent is to use these

    compounds as a sacrificial electrode layer during the electrokinetic

    deposition of methylmethacrylate monomer. Cylindrical reinforced

    concrete specimens were subjected to electrokinetic treatment and the

    specimens were tested to characterize porosity reduction and tensile

    splitting strength, showing an increase in the tensile strength. In addition,

    nine specimens treated electrokinetically and in long-term atmospheric

    exposure testing at NASAs Kennedy Space Centers seaside atmospheric

    exposure test site were tested to determine their corrosion rate.

    Abstract:

    In Situ Electrosynthesis of

    Polymethylmethacrylate within

    Ceramic Launch Pad Materials

    HEOMD

    http://www.nasa.gov/centers/kennedy/news/corrosion.htmlhttp://www.nasa.gov/centers/kennedy/news/corrosion.html
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    Adeyemi AdegbiteMorgan State University, MarylandMajor: Electrical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentors: Harry Shaw and Darryl Lakins

    The Satellite Network (SN) is a data communication system

    comprised of a constellation of Tracking and Data Relay

    Satellites (TDRS) and several ground terminals. My main

    purpose was attaining and organizing all the legal return

    service modes of the Narrow Band Modem and mapping them

    to each other, with proper documentation. The modes of the

    Narrow Band Modems are the different configurations that

    are being used during the various tests to check the

    functionality requirements. These modems are in use for theUSS-CR project, which will is testing key components that will

    replace current subsystems for the TDRS ground terminals at

    the White Sand Facility. Using requirement specification

    documents and test data, the modes are organized using

    Mindjet MindManager, a tool that is helpful for organizational

    and presentational purposes. With Mindjet, I successfully

    mapped all modes for a S-Band Single Access Return Service.

    Abstract:

    USS-CR Modem Functional

    Configuration Summary

    http://www.mindjet.com/http://www.mindjet.com/
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    Juan M. BarraganUniversity of El Paso at El Paso, TexasMajor: Mechanical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Johnson Space Center

    Mentor: Eric Hurlbert

    Morpheus is a vertical test bed that is currently being used

    by the NASA Johnson Space Center to explore and perfect

    green propellant propulsion. This vertical lander utilizes

    different technologies that allow the test bed to

    autonomously land, detect and avoid hazards with the help

    of various subsystems. The vehicle at the moment will be

    tested at the Kennedy Space Center and a spare vehicle is

    needed for backup. My task is to begin the construction of

    the spare vehicle propellant storage and propellant deliverysystem in conjunction with the vehicle structure, as well as

    supporting any testing and preparation for the KSC test.

    Learning from current vehicle testing, components new

    vehicles subsystem will be upgraded and modified for

    increased performance.

    Abstract:

    Morpheus Supportand

    Secondary Vehicle Development

    http://morpheuslander.jsc.nasa.gov/http://morpheuslander.jsc.nasa.gov/
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    The Neutron Star Interior Composition ExploreR (NICER) will be a NASA Explorer Mission of

    Opportunity, dedicated to the study of neutron stars, the only places in the universe

    where all four fundamental forces of nature are simultaneously important. Answering the

    long-standing astrophysics question How big is a neutron star?, NICER will confront

    nuclear physics theory with unique observation constraints, exploring the exotic states of

    matter within neutron stars, and revealing their interior and surface compositions through

    rotation-resolved X-ray spectroscopy. NICER will feature 56 co-aligned X-ray concentrators

    and matching detectors with a 2,000 cm2 effective area. Each optic is roughly 6 inches in

    height and 4 inches in diameter, featuring 24 concentric aluminum foils which are

    individually coated with gold. The detectors which are , located at the focal length of 1.085

    meters behind the optics, each have a 2mm aperture. NICER will be the first X-Ray

    telescope utilizing mirrors in a full cylindrical configuration, along with new

    manufacturing techniques on such a small scale. We began characterizing the

    effectiveness of the first assembled optics or engineering testing units (ETUs) bydetermining the point-spread function. The optics were placed inside a vacuum, where

    they received approximately parallel X-ray photons. The data is then picked up by the

    detector and analyzed with software. We find a 1.84 mm half-flux radius and a 3.49 mm

    80% flux radius for the fully populated optic, and a 0.72 mm half-flux radius and a 1.64 mm

    80 % flux radius for the sparsely populated optic. From these results we conclude that the

    optics are performing relatively well, and should meet design requirements with

    improvements in the manufacturing methods. (This project was co-authored by Billy

    Barrios, Steve Lentine, and Ceili Burdhimo).

    Goddard intern Billy

    Barrios performs an

    optical check on oneof the NICER Optics

    mirrors. Image

    Credit: URC.

    Abstract:

    NICER X-Ray Optics

    Assembly and Testing

    Billy BarriosCalifornia State University, Los Angeles, California

    Major: Mechanical Engineering/Physics

    Degree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Keith C. Gendreau

    SMD

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    Leishmaniases are among the most important emerging and resurging

    vector-borne diseases, second only to malaria in terms of the number ofaffected people. Leishmaniases are endemic in 88 countries worldwide

    and threaten about 350 million people (WHO, 2007). Since the first

    reported case of zoonotic cutaneous leishmaniasis (ZCL) in Saida, Algeria,

    in 1991, 1,275 cases have been recorded (Makhlouf & Houti, 2010), with

    the vast majority of study-area cases (99%) reported between the years

    of 2000 and 2009. An investigation of potential climatic indicators for the

    apparent shift in disease prevalence was conducted by comparing

    anomalies in the climate data specific to the local pathogen cycle. It was

    determined that long-term climate trends have resulted in conditions

    that promote the prevalence of ZCL. Increased precipitation haveresulted in greater vegetation and promoted host and vector population

    growth through a trophic cascade. Increased minimum temperatures

    have lengthened the annual duration of sandfly activity. Short-term

    variations in maximum temperatures, however. show a correlation with

    disease suppression in the subsequent years. These findings indicate a

    potential to forecast the risk of ZCL infection through models of the

    trophic cascade and sandfly population growth.

    Abstract:

    Incidence ofVector-borne Disease and Climate

    Change: A Case Study in Semi-Arid Algeria

    Tara BlakeyFlorida International University

    Major: HydrogeologyDegree Level: Ph.D.

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Lahouri Bounoua

    SMD

    http://www.ncbi.nlm.nih.gov/pubmedhealth/PMH0002362/http://www.ncbi.nlm.nih.gov/pubmedhealth/PMH0002362/
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    Quantum Cascade Lasers (QCLs) can be designed to operate anywhere from

    the Mid-IR to THz spectrum, and with their small size, tunable frequencies,and high energy output makes them an excellent choice for Trace Gas

    Detection. During the course of this internship, our job was to construct a

    laser system capable of producing low enough beat frequencies that could be

    detected via a spectrum analyzer. After the internship, the QCL would then

    undergo experimentation into detecting various molecules. Research and

    experimentation into QCLs will allow them to be used in both Earth science

    and future planetary NASA missions. QCLs are relatively new within the field

    of spectroscopy and operate on a principle different from that of common p-

    n junction diode lasers. In a diode laser, conduction band electrons jump into

    a valence band hole and emit a photon whose wavelength is determined by

    the band gap energy of the semiconductor, known as an interband transition.With QCLs, a conduction band electron can make a series of jumps in a

    staircase-like potential existing in the conduction band, emitting an identical

    photon in each transition. Here, a single electron emits a cascade of photons

    leading to the formation of a high-power laser. Transitions within a QCL take

    place from subband-to-subband inside a quantum well, continuing into the

    next quantum well, and so on. Thus, these are referred to as intersubband

    transitions.

    Abstract:

    Quantum Cascade Laser Frequency

    Modulation for Trace Gas Detection

    Harry Burton IIIDelaware State University

    Major: Applied OpticsDegree Level: Master of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Eduard Luzhanskiy

    SMD

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    Design, model, fabricate, setup, conduct and analyze thermal and

    cryogenic test results for several current JPL projects.

    Ultra Compact Imaging Spectroscopy (UCIS):

    Quantify the effective thermal conductance of a data cable to enable

    optimization of tactical cryocooler use in future systems.

    Airborne scanning MultiSPectral Infrared instrument (AirMSPI):

    Set up and run a test to determine whether normal operating thermal

    stresses on a silica filter will result in epoxy failure and

    delamination of the layers within the silica filter.

    Mars Atmospheric Trace Molecule Occultation Spectrometer (MATMOS):

    Created interface parts in Solidworks for the physical connection

    between the radiator, thermal strap and load; and created a LabVIEW

    data acquisition graphical user interface for the test data

    characterizing the cooling system thermal performance.

    Mechanical engineering

    researcher Kalind Carpenter

    assembles the SOLO TREC

    Power generation

    subsystem test rig. Image

    Credit: URC.

    Abstract:

    Thermal and Cryogenic

    Testing Systems Development

    Kalind CarpenterCalifornia State University, Los Angeles, California

    Major: Mechanical EngineeringDegree Level: Master of Science

    Intern Site: NASA Jet Propulsion Laboratory

    Mentor: Dr. Eugenio Urquiza

    SMD

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    Hygroscopic growth is one of the most fundamental properties of atmospheric aerosols.

    By absorbing or evaporating water, an aerosol particle changes its size, morphology,

    phase, chemical composition and reactivity, and other parameters such as its refractive

    index. Because of this, extensive research is being done on aerosol particle hygroscopic

    growth at NASA. This research is important to the understanding of aerosol effects on

    climate change. Currently, the operation of radiosondes is the most common technique

    used to characterize vertical profiles of temperature, water vapor mixing ratio and

    relative humidity. However, radiosondes are launched only two to three times a day

    because of the high cost of each one. The attempted solution to this problem is utilizing a

    Microwave Radiometer (MWR). Microwave radiometry allows for continuous retrievals

    of temperature profiles by measuring brightness and sky temperature at different zenith

    elevations. The focus of this study is the sensitivity of Relative Humidity Profiles obtained

    from both instruments. This will be accomplished by using temperature profiles from the

    MWR and radiosonde. The result of these comparisons will allow for the study of thesensitivity of the Relative Humidity profile obtained by radiosonde and those combining

    temperature profiles from the MWR and the Water Vapor mixing ratio from the

    radiosonde. These Relative Humidity profiles will then be compared to Relative Humidity

    profiles from the radiosonde. The data used in this study was acquired from the Howard

    University Beltsville Campus during the Discover AQ campaign in the summer of 2011.

    The result of this project will be used as a baseline for evaluating uncertainties in the

    retrieval of aerosol hygroscopic growth by means of Lidar measurement.

    Stanford Carter reviews

    data captured on the HURLRaman Lidar at the Howard

    University Beltsville Center

    for Climate System

    Observation. Image Credit:

    URC.

    Abstract:

    Study ofMicrowave Radiometer Temperature

    Profiles for Use in Calculating Relative Humidity

    Stanford CarterHoward University, Washington, D.C.

    Major: PhysicsDegree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Daniel Ramirez

    SMD

    http://meiyu.atmphys.howard.edu/beltsville/inde3.htmlhttp://meiyu.atmphys.howard.edu/beltsville/inde3.htmlhttp://meiyu.atmphys.howard.edu/beltsville/inde3.htmlhttp://meiyu.atmphys.howard.edu/beltsville/inde3.html
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    The Laser Interferometer Gravitational-Wave Observatory (LIGO) is a large-scale

    Michelson interferometer which aims to directly detect gravitational waves

    predicted by Albert Einstein in 1916. The gravitational waves sources that LIGO

    expects to detect consist of the merging of two neutron stars or a neutron and

    black hole at cosmic distances. It is anticipated that the coalescence of these

    compact objects may also produce a short -lived gamma ray burst (GRB).

    Unfortunately, LIGO is not accurate in localizing the points in the sky where the

    gravitational sources are to be found. The best that LIGO can do is to constrain a

    gravitational wave source in an area of approximately 100 square degrees,

    where literally millions of electromagnetic sources can be observed. So it seems

    that the simultaneous detection of gravitational and electromagnetic wavescoming from a source is highly unlikely. To facilitate the task of searching for

    electromagnetic counterparts coming from gravitational waves, a list of galaxies

    within 100 Mpc has been compiledthe gravitational waves galaxy catalog

    (GWGC). LIGO is now being designed to improve its sensitivity by a factor of 10,

    which means that it would be able to observe neutron star/ neutron star

    coalescence to distances of 300 Mpc and neutron star/ black hole coalescence

    up to 650 Mpc. Therefore, GWGC must be updated to contain galaxies at these

    distances. We present the results of the updates made to GWGC.

    Physics student Frank

    Ceballos discovers that

    work at NASA Goddard can

    be challenging, yet fun.

    Image Credit: URC.

    Abstract:

    Update: Gravitational Wave Galaxy Catalogue

    for the Rapid Search of Electromagnetic

    Counterparts from Gravitational Waves

    Frank CeballosUniversity of Texas at Brownsville, Texas

    Major: Physics

    Degree Level: Bachelor of Science

    Intern Site: NASA Glenn Research Center

    Mentor: Jonah Kanner

    SMD

    http://www.ligo.caltech.edu/http://www.ligo.caltech.edu/
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    Vanessa DoradoUniversity of Texas at El Paso, TexasMajor: Mechanical Engineering

    Degree Level: Master of Science

    Intern Site: NASA Marshall Space Flight Center

    Mentor: Kevin Pedersen

    Historically, spacecraft reaction control systems have primarily used cold gas

    thrusters because of their inherent simplicity and reliability. However, cold gas

    thrusters typically have a low specific impulse. It has been determined that a

    higher specific impulse can be achieved by passing a monopropellant fluid

    mixture through a catalyst bed prior to expulsion through the thruster nozzle.

    This research analyzes the potential efficiency improvements from using tri-

    gas: a mixture of hydrogen, oxygen, and an inert gas, in this case helium.

    Passing tri-gas through a platinum catalyst causes the hydrogen and oxygen to

    become reactive, ultimately heating the exiting fluid and generating a higher

    specific impulse. The goal of this project was to optimize the thrusterperformance by characterizing the effects of several system components. The

    performance effects were examined by varying catalyst types, catalyst lengths,

    and initial catalyst temperatures. Additional testing would utilize a hydrogen

    rich tri-gas mixture or characterize the performance effects of firing in a

    vacuum chamber for future applications and advancement in the field of green

    propellants

    Abstract:

    Characterization of a

    Tri-Gas Thruster

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    Jordan FuchsPrairie View A&M University, TexasMajor: Electrical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Johnson Space Center

    Mentor: Robert Hirsh

    My project involved improving upon existing software and

    developing new software for the Project Morpheus Team.

    Specifically, I created and updated Integrated Test and

    Operations Software (ITOS) user interfaces for on-board

    interaction with the vehicle during archive playback as well

    as live streaming data. These interfaces are an integral part

    of the testing and operations for the Morpheus vehicle,

    providing any and all information to evaluate instrumentsand ensure coherence and control during Morpheus

    missions. I also developed a bridge program for interfacing

    live CCSDS (telemetry) data to the Engineering DOUG

    Graphics Engine (EDGE) display for a graphical (stand-alone

    or VR dome) view of live Morpheus flights or archive replays.

    Abstract:

    ITOS to EDGE Bridge Software for the

    Morpheus Lunar/Martian Vehicle

    http://morpheuslander.jsc.nasa.gov/http://morpheuslander.jsc.nasa.gov/
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    Raul Garcia-SanchezHoward University, Washington, D.C.Major: Physics

    Degree Level: Ph.D.

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Paul Mahaffy

    The organic contaminants library was developed as part of the contamination control plan for the Mars

    Science Laboratory rover mission. Work to normalize the data taken from Sample Analysis at Mars (SAM)

    to match standardized organic compound databases such as the National Institute of Standards and

    Technology (NIST) is needed in order to increase its availability to other potential users. To do this, we

    analyzed a standard fragmentation pattern, in this case Perfluorotributyl amine (PFTBA), using the SAM

    GCMS settings that will be used for the actual mission and then calculated the ratio differences between

    the SAM PFTBA data and the NIST standard for PFTBA. This library is submitted as a New Technology

    Report, and will be readily available in the future. Carrying out a correction of the SAM spectral

    response, developing and providing an algorithm that makes these corrections to match with more

    standard libraries like NIST, will allow general users to use this library and correct SAM data for their

    work. The data is processed by correcting for instrumental calibration, and other specific instrumental

    behaviors. The processing is documented in a linked location related to the data directories. This works

    for a large number of the continuing satellite missions. The lower level data is primarily available from

    the mission operations groups. Although this work is intensive in terms of the GCMS Spectral library, the

    changes to the spreadsheets that contain entries supplementing the contaminants library should be

    minimal, and only needed when the normalization changes the spectra enough to change the chemical

    formula (in those cases the compound is properly identified by the library). With the expected data for

    the Mars Science Laboratory (MSL) Curiosity Mars landing being August 6, continued support of the

    mission via further library improvements will be needed.

    Raul Garcia-Sanchez and Dr. Prabhakar Misra with a model of

    the Sample Analysis at Mars (SAM) instrument for the Mars

    Science Laboratory (MSL) mission. Image Credit: URC. Abstract:

    Normalization of the

    SAM Spectra Using PFTBA

    http://marsprogram.jpl.nasa.gov/msl/http://marsprogram.jpl.nasa.gov/msl/http://marsprogram.jpl.nasa.gov/msl/http://marsprogram.jpl.nasa.gov/msl/
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    Serving another term as a cooperative program student at

    Marshall Space Flight Center, my tasks were largely varied

    within the EV32 Structural and Mechanical Design Branch.

    Within the branch, I helped provide structural and

    mechanical design support including: specialized engineering,

    technical assistance, program support, model and CAD

    packages for structural/mechanical component systems

    design, and development for spacecraft and vehicle systems.

    During this time I worked on efforts and projects that areproprietary and data sensitive and therefore not listed in

    detail here. Aside from these activities, I was being prepared

    for follow-on work and had to take course training and

    Preliminary Development Flight Instrumentation modeling as

    listed.

    University of Texas at El

    Paso Mechanical

    Engineering major Zenia

    Garcia. Image Credit:

    URC.

    Abstract:

    Principles in Avoiding Design Errors and

    Facets ofEngineering a Total System

    Zenia GarciaUniversity of Texas at El Paso, TexasMajor: Mechanical Engineering

    Degree Level: Master of Science

    Intern Site: NASA Marshall Space Flight Center

    Mentor: Kevin Pedersen

    SMD

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    Valeria C. Arce GonzlezUniversity of Puerto Rico, MayaguezMajor: Chemical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Glenn Research Center

    Mentor: Dr. Marisabel Lebrn-Coln

    Todays helicopter gearboxes are limited by their poor structural design and

    lack of capability to correlate changes in transmission and gearbox noise levels

    with expected changes in cabin noise levels. This research focuses on the

    development of multifunctional nanocomposite materials that possess high

    strength, good thermal conductivity and high-performance abilities in vibration

    and noise control. The project seeks to demonstrate improvement in the

    vibration damping properties of polymeric materials by the addition of carbon

    nanotubes. Carbon nanotubes are commonly used to improve the stiffness,

    durability, performance and damping properties of materials. Because of their

    adjustable elasticity and ability to act as springs, they can dissipate energy much

    more efficiently, becoming a key component in noise-reduction applications.

    Some of the greater benefits and payoffs of this research include quieter cabinsand the development of lightweight materials that carry no weight penalties.

    These materials have many other applications, especially in the automotive and

    aerospace industries where manufacturers require vibration-absorbing

    materials that are cost-effective for the production of next-generation vehicles.

    This research project involves the synthesis of epoxy nanocomposite materials,

    dispersion and organic functionalization of carbon nanotubes, and the

    processing and characterization of polymeric samples.

    Valeria C. Arce

    Gonzlez analyzes

    the dispersion of

    carbon nanotubes in

    an epoxy resin

    sample. Image

    Credit: URC

    Abstract:

    Effects ofCarbon Nanotubes Addition on

    Vibration Damping Behavior ofEpoxy Resins

    SMD

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    Climate variability in Australia is largely driven by an atmospheric phenomenon called the Southern

    Oscillation (SO), which involves a see-saw like behavior between low and high pressure systems within the

    equatorial Pacific regions. The interaction of SO with abnormally high sea surface temperatures (SSTs) El

    Nio and abnormally low SSTsLa Nia (anti-El Nio) creates extreme drought or extreme flooding,

    respectively, throughout Australia. El Nio-Southern Oscillation (ENSO) events have significant impacts on

    Australias landscape, ecosystems, agriculture production, and, as this report shows, human health. During

    La Nia years, when ENSO events involve increased rainfall and consequential flooding, Australias tropical,

    warm climate and an associated increase in vegetation growth from the rainfall creates an ideal habitat for

    mosquito population increases. Certain species of mosquitoes (Culux annulirostris) are carriers of Murray

    Valley Encephalitis (MVE) virus, a rare but potentially fatal infection that attacks neurological and muscular

    functioning. We hypothesized that a widespread increase in vegetation indicates an expansion of ideal

    mosquito production habitats and will translate to an increased risk of MVE contraction. Our objective is to

    show if a correlation exists between the ENSO-driven climate and consequential ecosystem changes and

    MVE outbreaks throughout Australia. This study makes use of the Moderate Resolution ImagingSpectroradiometer (MODIS) sensor operating on NASAs Terra satellite to obtain monthly Normalized

    Difference Vegetation Index (NDVI) data. It is assumed in this research that an anomalous increase in NDVI

    values indicative of vegetation growth occurs due to increased rainfall, which, in tandem with

    Australias tropical climate, allows for NDVI to be an adequate proxy for the combined influence of rainfall

    and temperature on mosquito ecology. Our results showed a general temporal and spatial correlation

    between MVE outbreaks and a greening period, suggestive of ideal mosquito breeding habitats and

    assumed population increases. (This project was co-authored by K.Cortney Gustafson, Mouhamad Diabate,

    and Dr. Assaf Anyamba).

    Kelly Gustafson marvels

    at the advance of

    technology while

    encountering archives ofresearch and equipment

    from ages past. Image

    Credit: URC.

    Abstract:

    Australia: Climate-Ecosystem

    Varability and Impacts on Diseases

    Kelly Courtney Gustafson

    Florida International UniversityMajor: Environmental Studies

    Degree Level: Master of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Assaf Anyamba

    SMD

    http://en.wikipedia.org/wiki/Southern_oscillationhttp://en.wikipedia.org/wiki/Southern_oscillationhttp://en.wikipedia.org/wiki/Southern_oscillationhttp://en.wikipedia.org/wiki/Southern_oscillation
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    Daniel H. Hernandez, Jr.University of Texas at El Paso, TexasMajor: Mechanical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Marshall Space Flight Center

    Mentor: Shane Brooke, Jon Street and Carolyn Russell

    Friction Stir Welding is a process in which different factors such as travel speed, rotational

    speed (RPM), and plunge force play a key role in creating a successful weld. Friction is

    created between two panels by a shoulder and pin. This friction causes the material at the

    abutting edge of two panels to plasticize (plastically deformed 70 percent of melting

    point- taffy consistency), allowing for the material to be stirred and welded. This project

    will consist of two separate but equally important tasks. First, is to analyze the nugget

    shape and material flow characteristics of conventionally friction stir welded (C-FSW)

    panels with different pin tool designs. Analyzing the nugget shape and stirring of the weld

    through optical microscopy will aid in understanding how these flats will affect a weld.

    There are six different pin tool designs for this project: a standard C-FSW pin without

    machined flat edges (baseline), and five others with flats ranging from 1 to 5. The panels tobe welded are aluminum 2219 to aluminum 2219. This project will aid in understanding the

    differences and similarities between each of the pins. This work will ultimately aid in

    determining which pin design provides the optimum weld schedule and characteristics.

    Second, is to support fixture design, stress analysis (FEA), and procurement for the Multi-

    purpose Crew Vehicle Stage Adapter (MSA) pathfinder cone to adapter ring weld for the

    Space Launch System (SLS). (The research was co-authored by Daniel H. Hernandez Jr. and

    Elvis Boves).

    Abstract:

    Stress Analysis, Fixture Design for

    MAS Pathfinder and Pin Tool Analysis

    Using Conventional Friction Stir Welding

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    Jesus HinojosaUniversity of Texas at Brownsville, TexasMajor: Physics

    Degree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Ronald Oliversen

    At the beginning of my internship, I operated the McMath-Pierce

    Solar Telescope at Kitt Peak National Observatory. There we

    observed the moon and received high-resolution spectral data of

    lunar exospheric sodium emissions for four nights. The overall data

    measured sodium emission from the lunar limb out to two lunar

    radii from the limb for lunar latitudes from the equator to the pole

    over lunar phases from the first to third quarter. Here at GSFC I

    have started gaining experience in CCD data reductions, line profile

    fitting, and IDL software programming. The expected outcome ofmy internship is to advance the understanding of the interaction

    between the solar wind and lunar surface via line profile

    measurements, yielding exospheric sodium atom temperatures and

    velocities.

    Abstract:

    Lunar Exospheric Sodium and

    Potassium Emissions

    http://nsokp.nso.edu/http://nsokp.nso.edu/http://nsokp.nso.edu/http://nsokp.nso.edu/
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    The Deep Space Network (DSN) is an international antenna network funded by NASA which

    provides communications and support for various space missions. A 34-meter beam

    waveguide antenna is under construction in Canberra, Australia, and requires a new downlink

    channel and telemetry processors. This project focuses on testing of new telemetry decoders

    which are implemented on Field-Programmable Gate Array (FPGA) boards. These are also

    intended to replace legacy telemetry processors in the future to improve ease of maintenance

    and sustainability. The intended functionality and performance of the decoders must be the

    same as those which they are replacing. The new decoders are tested using different code

    rates, coding schemes and modulation schemes standard to the DSN. The testing process

    utilizes equipment similar to those at DSN ground stations, along with a signal generator to

    provide equivalent RF signals. The Python scripting language is used to verify the integrity ofdecoded data and can handle large sets. These tools are used to obtain characteristics of

    performance such as symbol error rate (SER), bit error rate (BER), and signal-to-noise-ratio

    (SNR). Throughout the course of the internship, the encoding scheme that was of primary

    focus was Turbo Code using code rates and modulation schemes seen on the actual DSN.

    Discrepancies in decoder performance were encountered during testing, with several sources

    identified. Various parameters were added to the output to isolate different sections of the

    test setup for identifying those sources of error.

    Adrienne Lam with the

    telemetry processor and

    Unix computer. Image

    Credit: URC.Abstract:

    Testing ofFPGA Telemetry Decoders for the

    New 35 m Beam Waveguide Antenna

    Adrienne Lam

    California State University, Los Angeles, CaliforniaMajor: Electrical Engineering

    Degree Level: Master of Science

    Intern Site: NASA Jet Propulsion Laboratory

    Mentor: Dr. Chau M. Buu

    SMD

    http://deepspace.jpl.nasa.gov/dsn/http://deepspace.jpl.nasa.gov/dsn/
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    Alberto MataUniversity of Texas at Brownsville, TexasMajor: Physics

    Degree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Avi Mandell

    Using Interactive Data Language (IDL), an established data visualization

    software, I analyze infrared spectroscopic observations of protoplanetary

    disks. The observations are taken with the Very Large Telescope (VLT) in

    the Atacama Desert of Chile using the Cryogenic Infrared Echelle

    Spectrograph (CRIRES). Observing protoplanetary disks, or the gas and

    dust around early stars, gives us insight as to what material surrounds

    early stars, and since planets form in the protoplanetary disk of the star,

    investigating the chemical composition of protoplanetary disks allows us

    to probe the material that will eventually make up the planets around a

    certain star. Planets whose origins and compositions we would like to

    better understand include the recent discoveries of "super-Earths."

    Observing these super-Earths gives us minimal information as to what

    they are composed of, but observing protoplanetary disks can help us

    better understand the origins of the atmospheres and interiors of these

    planets.

    Brandon Norman (left) and University of Texas at Brownsville, TX student,

    Alberto Mata at the NASA Goddard Intern Poster Session. Image Credit: URC.

    Abstract:

    Investigating the Gas Chemistry of

    Protoplanetary Disks

    http://www.eso.org/public/teles-instr/vlt.htmlhttp://www.eso.org/public/teles-instr/vlt.html
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    Jose A. McKinnonUniversity of Texas at Brownsville, TexasMajor: Physics

    Degree Level: Master of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. John Baker and Dr. Jeffrey Livas

    Gravitational wave detectors in the mHz band (such as the Laser

    Interferometer Space Antenna, or LISA) will observe thousands of compact

    binaries in the galaxy which can be used to better understand the structure

    of the Milky Way. To test the effectiveness of LISA to measure the

    distribution of the galaxy, we simulated the Close White Dwarf Binary

    (CWDB) gravitational wave sky using different models for the Milky Way. To

    do so, we have developed a galaxy density distribution modeling code based

    on the Markov Chain Monte Carlo method. The code uses different

    distributions to construct realizations of the galaxy. We then use the FisherInformation Matrix to estimate the variance and covariance of the recovered

    parameters for each detected CWDB. This is the first step toward

    characterizing the capabilities of space-based gravitational wave detectors to

    constrain models for galactic structure, such as the size and orientation of

    the bar in the center of the Milky Way.

    Master of Science

    student Jose A.

    McKinnon.. Image

    Credit: URC.

    Abstract:

    Mapping the Milky Way Galaxy

    with LISA

    http://lisa.nasa.gov/http://lisa.nasa.gov/http://lisa.nasa.gov/http://lisa.nasa.gov/
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    In the last decade, there has been an

    increased interest in using palladium (Pd)

    nanostructures for hydrogen (H2) sensing

    devices. Nanostructured based sensors

    promise shorter response times and higher

    sensitivity due to their high surface-to-

    volume ratio. With this in mind, an anodic

    alumina membrane (AAM) Pd

    nanostructured based sensor has beendeveloped and tested. The Solid State

    Reduction method used formed a

    combination of a thin film and nanowires

    in the AAM. The fabrication method and

    preliminary test results are discussed here.

    Chemical engineeringdoctoral candidate

    Hctor Mendez-Colberg

    catches a rare moment

    of rest during his

    internship at NASA

    Glenn Research Center.

    Image Credit: URC.

    Abstract:

    Development of Chemical

    Sensors for Hydrogen Detection

    Hctor Mendez-ColbergUniversity of Puerto Rico, Mayaguez

    Major: Chemical Engineering

    Degree Level: Ph.D.

    Intern Site: NASA Glenn Research Center

    Mentor: Dr. Gary W. Hunter

    SMD

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    The Advanced Multimission Operations System (AMMOS) offers missions operationstools and services to deep space missions that are reliable and cost-effective. The

    Instrument Operations Subsystem (IOS) of AMMOS deals with the processing of data

    from space, and provides tools to orbiters and observatories for tactical operations

    related to image processing and instrument design. Currently, up to 189

    measurements from Mars' surface (such as wind speed, temperature, and

    atmospheric pressure) are available to observers in the form of raw data. However,

    this data is recorded every two seconds, making the amount of data enormous and

    more difficult to sift through for specific information. Using Javascript/jQuery, a more

    aesthetically pleasing way of viewing this information was developed and

    demonstrated to make it easier for scientists to dissect. Tools such as the Mars Image

    Viewer (MIV) are required from low-volume, relatively simple missions to high-volume, complex missions. Primary users of the MIV were observed in their workspace

    and surveyed. Secondary users were also queried on their interest in and the usability

    of the tool. The interaction between the MIV and its current/potential users were

    analyzed in order to define requirements and ensure that it adequately fit the needs

    of the users in ways that enable them to reach their goals with optimal efficiency.

    Recommendations were provided for the MIV users manual to further cater to the

    standpoint of the novice user.

    Kevin J. Monk II at

    California State

    University, Long Beach.

    Image Credit: URC.

    Abstract:

    Mars Image Viewer:

    User Needs Analysis

    Kevin J. Monk IICalifornia State University, Long Beach, California

    Major: Human Factors Psychology

    Degree Level: Master of Science

    Intern Site: NASA Jet Propulsion Laboratory

    Mentor: Elias Sayfi

    SMD

    http://ammos.jpl.nasa.gov/http://ammos.jpl.nasa.gov/
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    Gregory MoralesCalifornia State University, Long Beach, California

    Major: Human Factors Psychology

    Degree Level: Master of Science

    Intern Site: NASA Dryden Flight Research Center

    Mentor: Mark Pestana

    As part of the Federal Aviation Administration (FAA)

    Reauthorization Act, the FAA is tasked to develop regulations

    testing and licensing unmanned aircraft systems (UAS) to be

    integrated in the National Airspace System. Lead by NASAs

    Dryden Flight Research Center, a project is under way to address

    safety and operational challenges for UAS integration. The

    Research Ground Control Station is being developed as a test

    bed and database to provide data and proof of concept for a

    Ground Control Station. This research supports the developmentof standards and practices with consideration to human factors

    issues for the Ground Control Station. The project includes:

    developing and evaluation of display and control formats,

    command and control schemes, ergonomics, procedures for the

    UAS pilot, and other human system integration features.

    Abstract:

    Human Factors in

    Unmanned Aircraft Systems

    ARMD

    http://www.faa.gov/regulations_policies/reauthorization/http://www.faa.gov/regulations_policies/reauthorization/http://www.faa.gov/regulations_policies/reauthorization/http://www.faa.gov/regulations_policies/reauthorization/
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    This project involved Total Ionizing Dose (TID) tests at the

    GSFC radiation chamber. The tests were performed using

    a TLE2022 Bipolar Op Amp as the Device Under Test

    (DUT).

    The DUT was subject to a Cobalt 60 source at a Low Dose

    Rate (LDR). The main values observed were the input bias

    current, supply current, voltage offset, and current offset.

    The implication from the results support that the device

    has characteristics of radiation hardened.

    Intern BrandonNorman tests

    the op amp after

    taking it out of

    the radiation

    chamber of the

    Keithley 4200

    and HP test

    fixture. Image

    Credit: URC.

    Abstract:

    Low Dose Rate TID Testof

    Commercial Bipolar Op Amp

    Brandon NormanPrairie View A&M University, TexasMajor: Electrical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Jonathan Pellish

    SMD

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    Ryan OConnorCalifornia State University, Long Beach, California

    Major: Human Factors Psychology

    Degree Level: Master of Science

    Intern Site: NASA Ames Research Center

    Mentor: Dr. Walter Johnson

    The number of crew members in commercial flights has steadily

    decreased to two members, down from five members 50 years

    ago. The next step is to reduce the crew to one pilot, and

    eventually fully automate commercial aircraft, with one ground

    pilot managing numerous UAS. This reduction in crew will

    reduce costs for major airliners. Consistent development of new

    aeronautic technologies has enabled this drastic shift to be

    possible. The (FDRL) at NASA Ames is getting involved in theresearch efforts for the upcoming changes. My task as an intern

    was to develop a cognitive walkthrough and work directly with a

    commercial pilot to create testing scenarios and flowcharts for

    the experimental testing on single-pilot operations.

    Intern Ryan OConnor (left) with fellow California State

    University, Long Beach, graduate student Zack Roberts.

    Image Credit: URC.

    Abstract:

    Cognitive Walkthrough with a

    Commercial Pilotfor Preliminary

    Single-Pilot Operations Experiment

    ARMD

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    Edwin Ortiz-QuilesUniversity of Puerto Rico, Rio Piedras

    Major: Chemistry

    Degree Level: Ph.D.

    Intern Site: NASA Jet Propulsion Laboratory

    Mentor: Dr. William C. West

    Lithium ion batteries using Li2MnO3/LiMO2 (M = Mn, Co, Ni) as the cathode had

    been extensively studied. Under 0 C, batteries with this composite oxide present

    efficiency issues. This can be explained by a diffusion process with the lithium as

    consequences of the poor layer organization. LiCl salts can help improve this

    organization by resupplying the intercalated lithium to a molten mixture. Sensitivity

    studies directed to understand the effects of LiCl on the cathode material

    controlling variables as the synthesis time, and LiCl concentration will be

    accomplished. Electrochemical experiments using galvanostatic charge/dischargeprocesses at C/5 and C/10 and impedances at different temperatures provide direct

    information of the diffusion and the dynamics of the batteries prepared with

    Li2MnO3/LiMO2. Tap density analysis will be completed to have a better

    understanding of the behavior of the cathode after being packed in the batteries

    and an AlPO4 coating. Results show an improvement in the capacity of the cathode

    after the LiCl flux.

    Abstract:

    Molten Salt Flux Synthesis to Reduce

    Cation Disorder in Cathodes for Lithium

    Ion Batteries

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    Francisco PenaCalifornia State University, Los Angeles, California

    Major: Mechanical Engineering

    Degree Level: Master of Science

    Intern Site: NASA Dryden Flight Research Center

    Mentor: Dr. Lance Richards

    The Dryden Aero-Elastic Lab located at the AERO Institute is developing

    cutting-edge research in fiber optic strain sensing. The innovative fiber

    optics systems are capable of monitoring mechanical and thermal strains,

    which allow engineers to monitor real-time deformation of a structure.

    Utilizing the NASA University Research Center (S.P.A.C.E.) Uninhabited

    Air Vehicle (Odyssey) as a test bed for the fiber optics strain sensors,

    engineers will validate the capabilities of the Fiber Bragg Grating sensors.

    The use of finite element modeling will aid in the further development of

    embedded Fiber Bragg Grating sensors for Uninhabited Air Vehicles.

    With real-time, deformation-shape prediction, it will be possible toaccurately measure mode-shape deformations of aircraft wings due to

    aero-elastic effects on the aircraft during flight. Structural deformation

    data can be sent to a feedback control system to mitigate the aero-

    elastic effects on the airframe. Methods developed by NASA's Dryden

    Flight Research Center for real-time deformation-shape prediction of

    lightweight unmanned flying aerospace structures can potentially reduce

    the risk of in-flight breakups, such as that of the Helios Wing..

    Abstract:

    Analysis and Experimental Validation of

    Lightweight Structures for

    Uninhabited Aerial Vehicles

    ARMD

    http://aeroi.org/http://www.nasa.gov/centers/dryden/home/index.htmlhttp://www.nasa.gov/centers/dryden/home/index.htmlhttp://www.nasa.gov/centers/dryden/news/ResearchUpdate/Helios/Previews/index_prt.htmhttp://www.nasa.gov/centers/dryden/news/ResearchUpdate/Helios/Previews/index_prt.htmhttp://www.nasa.gov/centers/dryden/home/index.htmlhttp://www.nasa.gov/centers/dryden/home/index.htmlhttp://aeroi.org/
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    I have been working on the USS-CR (User Service

    Subsystem Component Replacement) Project that deals

    with the replacement of key components that process user

    signals within the TDRS (Tracking Data Relay Satellite)

    ground terminals at the White Sands Complex in New

    Mexico. New modems, Frequency Converters, Switch Gear,

    and a Monitor and Control System (MCS) are being

    provided to update Space Ground Link Terminals (SGLT)

    currently in use at White Sands. The main goal of USS-CR is

    to modernize equipment that is currently active and thenprovide backups so that hardware can stay functional until

    the SGSS (Space Network Ground Segment Sustainment)

    project is complete around the year 2017. In particular, my

    research involves learning various Systems Engineering

    techniques so that I can model a SSAF (S-band Singe Access

    Forward) service.

    Morgan State

    electrical

    engineering

    student DarianPhillips. Image

    Credit: URC.

    Abstract:

    Modeling a SSAF Service

    Darian PhillipsMorgan State University, Maryland

    Major: Electrical EngineeringDegree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Harry Shaw

    SMD

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    Zachary RobertsCalifornia State University, Long Beach, CaliforniaMajor: Human Factors Psychology

    Degree Level: Master of Science

    Intern Site: NASA Ames Research Center

    Mentor: Dr. Walter Johnson

    Using a simulated air traffic environment, this study

    measured the response time, execution time, and

    general behavior of unmanned aerial vehicle (UAV)

    pilots in response to direct commands from air traffic

    controllers. Data was collected from eight participant

    UAV pilots who were asked to respond to and execute

    ATC commands as quickly as possible. Quick

    responses to ATC commands are one factor essential

    for UAVs to operate safely with manned aircraft andthis measured response data contributes to the

    knowledge base necessary to fully integrate

    unmanned aerial systems into the national airspace

    in the near future. (This project was co-authored by

    Zachary Roberts and Jason Ziccardi).

    Abstract:

    Measured Response to

    UAS Pilot Commands

    ARMD

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    An experimental study was conducted on the Mid-Atlantic region to investigate the rainfallvariability within the instantaneous field of view of the microwave sensor-based satellite rainfall

    estimate. The study was conducted through 30 rain gauges that were deployed at 11 sites, where

    eight sites had triple and remaining sites had dual gauges. The gauges were tipping bucket at 0.01

    inches resolution. The time of the t ip was recorded to a data logger which is powered by lithium

    battery. A continuous gauge record was obtained at every gauge site from May 2005 to September

    2010. The gauges sites were distributed from Ocean City, Maryland, to Kiptopeke, Virginia, at a

    maximum separation of 150 km and at a minimum separation of 1 km between the two sites at

    Wallops Island, Virginia. This study focuses on the variability of rainfall at different climatological

    periods. The observations were divided into 20 seasons, 10 cold/warm periods, and five years. A

    stretched exponential model was applied to the correlations of paired gauge rainfall at 30-minute

    integration period. Two tips (0.5 mm) were considered as the threshold for rain events. The

    correlations fell below 50 % at a 10 km distance most of the time in an observational period, whilethey were below 20% at 40 km distance. The variability was more noticeable between the seasons

    than between the warm/cold periods and between the years. This could, in part, be related to the

    sample size, partly to differences in rainfall characteristics. Additionally, the remnants of tropical

    cyclones bring abundant rainfall to the Mid-Atlantic region but they may not be observed at a given

    year. The nugget parameter was mainly above 0.95, while the shape parameter was mainly

    between 0.4 and 1.0. The correlation distances remained mostly less than 50 km at a given

    observational period.

    Rigoberto Roche makes

    changes to improve

    output statistics and

    provide high quality

    graphical represen-

    tations of the analyzed

    data produced during

    his internship at NASA

    Goddard Space Flight

    Center. Image Credit:NASA/Dr. Ali Tokay.

    Abstract:

    An Experimental Study of the

    Small-Scale Variability of Rainfall

    Rigoberto RocheFlorida International University

    Major: Biomedical Engineering, Mechanical Engineering

    Degree Level: Master of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Ali Tokay

    SMD

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    Robert Conrad RorieCalifornia State University, Long Beach, CaliforniaMajor: Human Factors Psychology

    Degree Level: Master of Science

    Intern Site: NASA Ames Research Center

    Mentor: Dr. Walter Johnson

    This study examined the effect of force feedback on target

    acquisition in a simulated task, using a computer mouse

    and the Novint Falcon, with and without force-feedback

    information. Participants were asked to select targets that

    varied in size, distance, and angular direction from the

    start location. Results showed significant differences

    between the movement times for the various input

    devices. Movement times with the mouse and the Falcon

    with force feedback were significantly faster than the

    Falcon without force feedback. Force feedback was foundto reduce the effect of target size, but not the effect of

    target distance. Force feedback also produced faster

    movement times when the direction of movement was in

    two dimensions. The findings suggest that force feedback

    may be a useful method for assisting pilots in future CDTIs.

    Abstract:

    EffectofForce Feedbackon an

    Aimed Movement Task

    ARMD

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    Janet RuedasPrairie View A&M University, TexasMajor: General Engineering, Emphasis on Chemical Engineering

    Degree Level: Master of Science

    Intern Site: NASA Johnson Space Center

    Mentor: Dr. Ramona Gaza

    When charged particles pass through CR-39 detectors, they lose

    energy and break the molecular bonds of the CR-39 polymer to form

    paths of high chemical reactive sites along their trajectories. These

    trajectories can be revealed as etched cones on the surfaces of CR-39

    detectors by chemical etch for a CE-39 plate. Chemical etching for

    plastic nuclear track detectors (CR-39) and thermoluminescence

    measurements were performed per established techniques currently

    used by the Space Radiation Analysis Group (SRAG) at NASA/JSC.

    Work objectives included: working with the sodium hydroxide (NaOH)

    etching solution, etching the plastic nuclear track detectors,measuring the detectors pre- and post-etch. The goal was to

    calculate the bulk etch and prepare the detectors for storage for

    future analysis. Over 150 CR-39s were etched successfully and the

    bulk etch values were analyzed for accuracy using the standard errors

    and error propagation..

    Prairie View A&M

    University

    researcher Janet

    Ruedas engraves

    CR-39 detectors foretching. Image

    Credit: URC.

    Abstract:

    Chemical Etching ofPlastic

    Nuclear Track Detectors

    ARMD

    http://srag-nt.jsc.nasa.gov/http://srag-nt.jsc.nasa.gov/
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    The sustainability of aviation directly depends on the availability ofenvironmentally responsible fuel. With the growing gap between petroleum

    production and demand, increasing prices, carbon emissions, mounting

    environmental regulations, and the limited concentration of known fuel

    reserves in politically unstable regions, biofuels are considered a viable

    alternative to securing the future of aviation. Biofuels are a renewable

    energy source, which could be customized to meet specific fuel needs.

    NASA GRC developed the GreenLab Research Facility to study two principal

    sources of biofuels: arid land halophytes (salt-tolerant plants) and sea water

    algae. Through a Life Cycle Assessment (LCA) of the GreenLab, we

    investigated the benefits and contributions to motivating the nextgeneration in STEM-related fields that the facility and its research offer

    outweighs the cost of running the program every year. We also looked into

    the optimization of Chaetomorpha sp. macro-algae by studying its growth

    under four different conditions. Results showed that a direct light source

    and some dirt accumulation lead to more successful growth of

    Chaetomorpha sp. macro-algae

    Kimberlin Schnittakercleans and monitors the

    six ecosystems for

    optimal growth of

    halophytes (salt-tolerant

    plants) used for the

    creation of biofuels.

    Image Credit: NASA

    Glenn/Tamaera

    McDowell.

    Abstract:

    A Life Cycle Assessmentof a Self-Sustainable

    Renewable Energy Ecosystem

    Kimberlin SchnittakerUniversity of Texas at El Paso, Texas

    Major: Metallurgical and Materials Engineering

    Degree Level: Master of Science

    Intern Site: NASA Glenn Research Center

    Mentor: Dr. Bilal Mark McDowell Bomani

    SMD

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    Christopher St. JulianPrairie View A&M University, Texas

    Major: Electrical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Johnson Space Center

    Mentor: Chatwin Lansdowne and Brandon Sherman

    The aim of this project is to demonstrate techniques for effectively penetrating

    a radio-shielded enclosure using Ethernet cable (CAT-6). This process requires

    that we measure the shielding performance by means of testing and data

    orchestration to collect and analyze our data, and then present observations

    with different test cases. Each test case would represent a different penetration

    strategy that utilizes distinctive wire coupling and characteristics (i.e., the type

    of bulkhead link, the twist of each CAT-6 cable, the shielding type of each CAT-6

    cable, and the length of the cable). As the different cable setups are fabricated,

    a prototype evaluation of setup is conducted to measure the signal integrity of

    the testing configuration. Our signal integrity is measured through the analysisof different parameters found in the prototype evaluation such as RF leakage,

    impedance mismatch, and decay rate. As data values are effectively collected

    and analyzed, the most effective cable setup is selected based upon its ability to

    penetrate the shielded enclosure. The testing data are compared in conjunction

    with the cost of the manufacturing of the prototype wire penetration.

    Abstract:

    Evaluate Techniques for Penetrating a

    Radio-Shielded Enclosure

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    When irradiating an Advanced Micro Device(AMD) Processor that is connected to the

    motherboard within a chamber, it is

    important to shield the motherboard from

    the gamma rays. In doing so I constructed a

    collimator with lead (Pb) bricks so that only

    the AMD processor is open to the gamma

    rays. While the motherboard was powered,

    the AMD processor experienced radiation.The results examined the effects that

    radiation had on an AMD processor and

    whether or not the processor could survive

    in the harmful space radiation environment.

    Eric Thomas, is a

    mechanical engineering

    major at Prairie ViewA&M University. Image

    Credit: URC

    Abstract:

    Radiation Testing on Biased

    Commercial AMD Microprocessor

    Eric ThomasPrairie View A&M University, Texas

    Major: Mechanical Engineering

    Degree Level: Bachelor of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Jonathan Pellish

    SMD

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    Lithium-ion batteries are among the most energetic rechargeable batteries available,

    making them very popular for various applications. A lithium-ion rechargeablebattery provides high energy density, requiring less weight and smaller size

    compared to other rechargeable systems. The battery manufacturer ABSL selected

    the Sony Lithium 18650 HC cell in the late 1990s to make its space-qualified cells.

    NASA Goddard Space Flight Center has flown ABSL batteries built from Sony 18650

    HC cells on ST-5, SDO and LRO missions. Recently, Sony made modifications to these

    cells due to failures in terrestrial applications. The addition of a mandrel tube is

    supposed to "improve the vent path within cell to the safety vent" (Troutman, Joe,

    2011) without causing any changes in the performance of the cell and the built-in

    safety features. The aim of my project was to establish the baseline characterization

    of the life-test batteries, which the contractors at the Naval Surface Warfare Center

    at Crane, Indiana, will use to compare later performance tests of the Sony 18650 HC

    and Sony 18650 HC mandrel cells. The study consisted in the creation of a test planthat allows researchers to know the capacity of the battery and its behavior in

    different environments. The test plan was conducted in the Battery Laboratory at

    NASA Goddard Space Flight Center. The project exposed me to Integration and

    Testing (I&T) in a Class 10,000 clean room, visits to contractors and vendors (SAFT,

    ABSL), and the opportunity to travel to the Naval Surface Warfare Center at Crane,

    Indiana. (This project was co-authored by Loraine Torres-Castro, Leonine S. Lee,

    Thomas Y. Yi and Ram S. Katiyar).

    Ph. D. candidate Loraine Torres-Castro tests the batteries for the Global PrecipitationMeasurement mission. Image Credit: URC.

    Abstract:

    Global Precipitation Measurement Mission Project

    Life-Test Support/Life Test Battery Characterization

    Loraine Torres-CastroUniversity of Puerto Rico, Rio Piedras

    Major: Physical Chemistry

    Degree Level: Ph.D.

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Amri Hernndez-Pellerano

    SMD

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    The overall objective is to assess the potential of satellite Lidar to retrieve thesurface of the coastal tides during normal (non-surge) conditions. Specific

    objectives are to assess the capability of the GLAS sensor on board the ICESat

    satellite platform to retrieve the spatial water surface profile during a March 2006

    transect over the Chesapeake Bay, using the 1064 wavelength; validate the

    retrieved water levels using a calibrated, high resolution 2D hydrodynamic model;

    and provide insight on future altimetry observations of coastal regions using Lidar.

    The present study focuses specifically on the capability to retrieve water surface

    elevations of the Chesapeake Bay during a single ICESat transect in March 2006.

    Validation is achieved using water surface elevations with a calibrated 2D, high-

    resolution hydrodynamic model. This is because ICESat observations do not fall

    exactly over available in situ tidal gages. Thus, it is necessary to first calibrate themodel using tide gages. Then, one can compare the ICES at elevations to those grid

    elements over which the satellite observations occur. Future Lidar altimeters, that

    will provide higher vertical precision and spatial coverage, should be of significant

    benefit not only to hydrodynamic modelers, but also to a wide range of

    applications including water resources planning, weather forecasting, ecosystem

    monitoring, and disaster prevention and management.

    Florida International

    University

    Environmental

    Engineering major

    Viviana Villamizar.

    Image Credit: URCAbstract:

    Assessment of ICESat Altimetry and Tidal

    Gage Water Elevations with Hydrodynamic

    Model Predictions for the Chesapeake Bay

    Viviana VillamizarFlorida International University

    Major: Environmental Engineering

    Degree Level: Master of Science

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Michael F. Jasinski

    SMD

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    Geiger-mode avalanche photodiodes (APDs) canconvert the arrival of a single photon into a

    digital logic pulse. Arrays of APDs can be directly

    interfaced to arrays of per-pixel digital

    electronics fabricated in silicon CMOS, providing

    the capability to time the arrival of photons in

    each pixel. These arrays are of interest for

    "flash" LADAR systems, where multiple target

    pixels are simultaneously illuminated by the

    laser during a single laser pulse, and the

    imaging array is used to measure range to each

    of the illuminated pixels. This summer I planned

    to integrate the GM-APD camera with a Yb:YAG

    laser for experimental test of LIDAR and

    distance-imaging.

    Michael Joseph Williamsreceived the Award of

    Excellence for his

    research poster at the

    2012 NASA Summer

    Intern Symposium.

    Image Credit: URC.

    Abstract:

    Geiger Mode APD 1-Kilopixel Camera

    for 3-D Topographic Mapping

    Michael Joseph Williams

    Delaware State UniversityMajor: Optics

    Degree Level: Ph.D.

    Intern Site: NASA Goddard Space Flight Center

    Mentor: Dr. Anthony Yu

    SMD

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    Jason ZiccardiCalifornia State University, Long Beach, CaliforniaMajor: Human Factors Psychology

    Degree Level: Master of Science

    Intern Site: NASA Ames Research Center

    Mentor: Dr. Walter Johnson

    Using a simulated air traffic environment, this study

    measured the response time, execution time, and

    general behavior of unmanned aerial vehicle (UAV)

    pilots in response to direct commands from air

    traffic controllers. Data was collected from eight

    participant UAV pilots who were asked to respond to

    and execute ATC commands as quickly as possible.

    Quick responses to ATC commands are one factor

    essential for UAVs to operate safely with mannedaircraft and this measured response data

    contributes to the knowledge base necessary to fully

    integrate unmanned aerial systems into the national

    airspace in the near future. (Jason Ziccardi and

    Zachary Roberts, co-authors)

    California State

    University student

    Jason Ziccardi.

    Image Credit: URC.

    Abstract:

    Measured Response to

    UAS Pilot Commands

    ARMD

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    With sincere appreciation, the National Aeronautics and Space Administration

    acknowledges the talent, hard work and dedication to excellence of those whose

    contributions have resulted in the success of the NASA University Research

    Centers Virtual Poster Session and Symposium.

    NASA Summer MentorsDr. Assaf Anyamba, Dr. John Baker, Dr. WilliamBluethmann

    Dr. Bilal Bomani, Dr. Lahouari Bounoua, Dr. Chau Buu, Dr.Luz Calle, Shirley Chung, Dr. Amber Emory, Dr. RamonaGaza

    Dr. Keith Gendreau, Jeffrey George, Amri Hernndez-Pellerano

    Robert Hirsh, Dr. Gary Hunter, Eric Hurlbert, MichaelJasinksi

    Dr. Walter Johnson, Dr. Alicia Joseph, Jonah Kanner

    Dr. Michael Krainak, Darryl Lakins, Chatwin Lansdowne

    Dr. Marisabel Lebrn-Coln, Leonine Lee, Dr. Jeffrey Livas

    Eduard Luzhanskiy, Dr. Paul Mahaffy, Dr. Avi Mandell

    Dr. Ronald Oliversen, Kevin Pedersen, Dr. Jonathan Pellish

    Mark Pestana, Dr. Daniel Ramirez, John Redmon, Dr. LanceRichards, Carolyn Russell, Elias Sayfi, Harry Shaw, JonStreet, Dr. Ali Tokay

    Dr. Eugenio Urquiza, Dr. William West, Anthony Yu

    NASA Education StaffDr. Penny (Madonna) Adams (JSC), Dr. Lenell Allen (JPL)

    Bernice Beznoska (GRC), Candance Clements (DFRC)

    Benita Desuza (KSC), Dr. David Kankam (GRC)

    Darla Kimbro (Headquarters), Maria Lopez (ARC)

    Kathleen Powell (LRC), Diego Rodriguez (JSC)

    Dr. Nathan Sovik (SSC), Jenny Tieu (JPL), Vanessa Webbs

    (GRC)

    NASA Center Technical Officers

    Brenda Collins (ARC), Dr. Marilyn Lewis (MSFC), Misti

    Moore (JSFC), Janie Nall (GSFC), Joeletta Patrick

    (Headquarters)

    Dr. Thomas Pinelli (LRC), Dr. Lance Richards (DFRC)

    Darlene Walker (GRC)

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    Acknowledgements (Continued)

    University Research Center Faculty and Staff

    California State University, Long Beach

    Dr. Thomas Strybel, Project Director

    Dr. Kim-Phuong Vu

    Diandra Porter

    California State University, Los Angeles

    Dr. Helen Ryaciotaki-Boussalis, Project Director

    Dr. Darrell GuillaumeDr. Charles Liu

    Daisy Lui

    Delaware State University

    Dr. Noureddine Melikechi, Project Director

    Teresa Curto

    Jacquelyn Jones

    Dr. Renu Tripathi

    Florida International University

    Dr. Fernando Miralles-Wilhelm, Project Director

    Juan Rodriguez

    Howard University

    Dr. Everette Joseph, Project Director

    Katherine Cooke-Mundle

    Teria Powell

    Dr. Demetrius Venable

    Morgan State UniversityDr. Carl White, Project Director

    Albert Sweets

    North Carolina A&T State University

    Dr. Kunigal Shivakumar, Project Director

    Latoya Best

    Dr. Vinayak Kabadi

    North Carolina Central University

    Dr. Branislav Vlahovic, Project Director

    Sergei Shendrick

    Dr. Marvin Wu

    Prairie View A&M University

    Dr. Richard Wilkins, Project Director

    Frank (Pat) Craddock

    Dr. Kirby Kelvin

    Carolyn Wedeking

    University of Texas at Brownsville

    Dr. Mario Diaz, Project Director

    Leslie GomezMaribel Gonzalez

    Robert Stone

    Texas Southern University

    Dr. Adebayo Oyekan, Project Director

    Brandi Butler

    University of Puerto Rico, Rio Piedras

    Dr. Carlos Cabrera, Project DirectorDr. Ana-Rita Mayol

    Omayra Rivera

    University of Texas at El Paso

    Dr. Ahsan Choudhuri

    Laura Barnum

    Nathaniel Robinson

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    Acknowledgements (Continued)

    URC Project Management TeamKatrina Y. Emery

    Chief, Office of Education

    NASA Dryden Flight Research Center

    University Research Centers National Project

    Manager

    Debra Weathers

    University Research Centers Project

    Administrator

    Tyra Wheeler-Zubia

    University Research Centers Project

    Associate for Evaluations/Communications

    Daesha Roberts

    University Research Centers Project Assistant

    Kaitlin Wright

    University Research Centers Summer Intern

    Judges Event PlanningCommittee and

    Support Staff

    For more information regarding the University Research Centers, please visit our website at

    http://www.nasa.gov/offices/education/programs/national/urc/home/index.html

    and follow us on Facebook at:

    Sarah Brown

    Frank (Pat) Craddock

    Noelle Coley

    Katrina Emery

    Dr. Kelvin KirbyJane Nall

    Joeletta Patrick

    Daesha Roberts

    Nate Robinson

    Diego Rodriguez

    Dr. Thomas Strybel

    Debra Weathers

    Tyra Wheeler-Zubia

    Jeffery Livas

    Janice Makinen

    Dr. Prabhakar Misra

    Joseph Muniz

    Dr. Oscar Murillo

    Ronald Oliversen

    Jonathan Pellish

    Dr. Lance Richards

    Nate Robinson

    Rene Sanchez

    Jennifer Scott-Williams

    Heather Smith

    Dr. Kim Vu

    Stephen Alter

    Vernol Battiste

    Sayak Biswas

    Damon Bradley

    Heidi Brewer

    Dr. Carlos Cabrera

    Terence Doiron

    Elena Fermin

    Darryl Gaines

    Dr. Hashima Hasan

    Dr. Daryush Ila

    Dr. Kiranmayee Kilaru

    Kurt Kossel

    Dr. Ray Ladbury

    Darryl Lakins

    Dr. Marilyn Lewis

    http://www.nasa.gov/offices/education/programs/national/urc/home/index.htmlhttp://www.nasa.gov/offices/education/programs/national/urc/home/index.htmlhttp://www.nasa.gov/offices/education/programs/national/urc/home/index.html