NASA ISGC Fellowship
Application Deadline: March 8, 2024
Thank you for your interest in applying for the NASA Idaho Space Grant Consortium 2024-2025 Graduate Fellowship.
Each fellowship is worth $44,000 and is good for one year.
Applications must be completed by March 8, 2024.
Letters of Recommendation must be submitted by March 8, 2024.
You must be a U.S. Citizen and full-time student to apply.
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Please note that once you start the application, you will not be able to open it back up to make changes. With that in mind, we strongly recommend that you have the following prepared before completing the application:
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Current resume
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Latest unofficial transcript
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Research proposal
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Contact information for two letters of recommendation
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Your research proposal must include:
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Title Page with date of submission, title of project, and an abstract briefly describing the proposed research
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Description of proposed research to include the goals, methods, and expected outcomes.
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Research timeline
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Alignment with NASA's current activities
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Publication Plan
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References
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(Optional) Previous ISGC Fellowship support
The Research Proposal should not exceed 5 pages, excluding references, title page, and previous ISGC Fellowship support information.
Your proposal will be evaluated based on how well it addresses the following criteria; ranking weight used during evaluation of applications is in parenthesis:
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Merit of proposed research (40%) - Are the goals of the research attainable? Are the proposed methods feasible?
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Research timeline (10%) - Is it feasible to complete the research within the 1 year fellowship timeline? Are tasks and milestones clearly articulated?
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Alignment (20%) - Is the proposed research aligned with NASA's Strategic Goals and/or the goals of the ISGC?
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Publications (10%) - Is there a publication plan? Is it reasonable?
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Two letters of recommendation (20%)-. One of these must come from your Research Advisor who will be supporting you during your award period.
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Proposals will be reviewed based on these elements, and final funding decisions will be based on recommendations by the review team to the Program Director.
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Please send each of your recommending parties the following link to fill out:
https://app.smartsheet.com/b/form/1dfe7b3fcaef4d00b9f090d59d5aa407
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An informational webinar will be held:
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Thursday, January 11th at 5:00 pm Pacific /6:00 pm Mountain​
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Join Zoom Meeting
https://uidaho.zoom.us/j/82115526084
Meeting ID: 821 1552 6084 -
A recording of the webinar will be posted
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If you have any questions, please reach out to us at isgc@uidaho.edu
2021-2022 Fellowship Awardees
Will Weygint
M.S., Department of Natural Resources and Society
University of Idaho
Rodrigo Padilla
Ph.D, Department of Mechanical Engineering
University of Idaho
Determining the suitability of thermal remote sensing for monitoring intra-annual tree growth in subalpine conifer forests of Idaho and the Intermountain West
Abstract:
Climate change-related shifts in hydrologic regimes are altering water availability in snowdominated ecosystems throughout Idaho and the Intermountain West. Of particular importance is increasing variability in the amount and duration of winter snowpack in subalpine forests and its
effects on tree wood growth, which provides important ecosystem services including wood production, habitat provisioning, and carbon sequestration. Due to its linkages to water availability tree wood growth could also be estimated using in-situ, airborne, and satellite leaf temperature measurements. The main goal of this project is to further explore linkages between tree wood growth and leaf temperatures to determine the suitability of using remotely sensed conifer shoot and canopy temperature (TS and TC, respectively) measurements as a proxy for intra-annual tree wood growth in subalpine forests. The two major objectives of this project are: 1) Explore feedbacks between TS and diurnal tree wood growth dynamics, and 2) test the spatial
scalability of the relationships between temperature and growth using unmanned aerial vehicle (UAV)-determined TC as well as satellite data products. This project will utilize in-situ data collected from an existing environmental monitoring network within the University of Idaho Nokes Experimental Forest near McCall, Idaho, as well as satellite TC measured from the ECOsystem Spaceborne Thermal Radiometer Experiment on Space Station (ECOSTRESS), a NASA instrument designed to collect surface temperature measurements across the globe. Results from this project will provide researchers and managers with a novel approach for monitoring the effects of climate change-induced alterations in hydrologic variability on tree wood growth in subalpine forests in Idaho and the Intermountain West. Idaho Space Grant Consortium Fellowship funding would be used to start this project and to complete analysis of objective 1 during the 2021-2022 academic year.
On the Aerodynamics of Fluid Structure Interaction
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Abstract:
An experimental study is being proposed to better understand flutter near the velocity instability range. Experiencing flutter is undesirable for aircraft in flight as it causes structural fatigue and failure, as well as contributing a large increase in drag. This phenomena will directly impact the efficiency of aircraft performance which is not desirable for the recent NASA project, Advanced Aerodynamic Design Center for Ultra-Efficient Commercial Vehicles. The scenario of ultra-efficient high-aspect wings is idealized to a cantilevered membrane to allow for a controlled experimental approach. Particle Image Velocimetry will be used to measure the velocity field that will be triggered along with load measurements experienced by the membrane on a corresponding time series. Hot Wire Anemometry will also be used to profile the wake of the membrane similarly be triggered with load measurements. This will allow to further quantify the pressure differential and the vortex shedding from a stable state to a uttering state. These measurements will help understand the causes of sudden flutter that will aid in validating models for these types of systems. Being able to understand these types of system will also help improve the design process for efficient aircrafts.