Project Grant NNX15AP65H
- This $422,259 Project Grant award from the National Science Foundation's (NSF) Computer and Information Science and Engineering (CISE) program (CFDA 47.070) will fund the development of a novel "Spherical Sailing Omnidirectional Rovers" (SSAILORS) technology. The primary objective is to establish the first spherical, wind-powered rover capable of moving in all directions, enabling persistent and autonomous characterization of remote environments. Through a combined physical and control...
- This $272,400 federal Project Grant award from the National Science Foundation (NSF) Engineering program (CFDA 47.041) supports a collaborative research effort between the University of California, Los Angeles (UCLA) to investigate and develop techniques for estimating and controlling gust-induced aerodynamic effects in energy and propulsion systems involving lifting surfaces. The key objectives of the 18-month project are to leverage prior research on unsteady aerodynamics to advance the...
- This Project Grant award, funded by the National Science Foundation (NSF) under the Engineering program (CFDA 47.041), supports research to develop a miniaturized Sagnac gyroscope using integrated photonics on a lithium tantalate platform. The $472,120 award to Carnegie Mellon University aims to enhance the sensitivity and stability of these compact optical gyroscopes, which have applications in navigation systems, drones, and virtual/augmented reality. The project explores the use of...
- This Early-concept Grants for Exploratory Research (EAGER) award from the National Science Foundation's (NSF) Integrative Activities (IA) program, CFDA 47.083, provides $149,980 to the University of Maine System to conduct research on the orbital motion dynamics of offshore wind turbines (OWTs) during the installation phase. The interdisciplinary project team will investigate the unique dynamics of partially installed bottom-fixed OWTs using wave tank experiments and high-fidelity numerical...
- This $255,843 National Science Foundation project grant under the Technology, Innovation, and Partnerships program will fund research and development of an integrated high lift propulsor to enable affordable and energy-efficient advanced air mobility aircraft designs. Wayfarer Aircraft Research and Development Inc. will conduct wind tunnel experiments and computational fluid dynamics simulations from August 2022 to July 2023 to characterize aerodynamic interactions between a propeller and wing...
- Seaflight Technologies Inc. will develop novel aerodynamic circulation control technologies for electric aircraft wings through this $275,000 National Science Foundation Project Grant awarded under the NSF Technology, Innovation, and Partnerships program (CFDA 47.084). The one-year project will advance research and development of high-lift wing designs using electric jet circulation control to increase maximum lift coefficients and enable longer range for small electric aircraft. Computational...
- The National Science Foundation (NSF) awarded a $272,800 SBIR Phase I Project Grant to Morningbird Media Corporation to develop and test a prototype propulsion engine that utilizes electromagnetic energy to enable high-speed space travel. The goal is to create a fundamentally new approach to spacecraft propulsion that could lead to orders of magnitude faster space travel compared to current chemical propulsion systems. The key technical objectives are to develop a complex dielectric material and...
- This Project Grant award from the National Science Foundation's (NSF) Engineering program (CFDA 47.041) will support $300,000 in research towards the development of millimeter-scale flying robots capable of controlled operation without a physical connection for power or data. The project aims to create robots powered and controlled remotely by a single-axis alternating magnetic field, with careful design of the flying structures to provide passive aerodynamic and gyroscopic stability. The...
- This Project Grant award from the National Aeronautics and Space Administration (NASA) under the Space Technology program (CFDA 43.012) provides $249,781.00 to the Regents of the University of Minnesota to conduct research on a "Concept Demonstration of Directed Energy Propulsion with Metasurface Lightsails". The 3-year project, which began on May 19, 2025 and is scheduled for completion by May 18, 2028, aims to advance transformational space technologies that can enhance NASA's...
- This Project Grant award from the National Science Foundation's Geosciences Program (CFDA 47.050) provides $589,888 to the Space Science Institute (SSI) to conduct a series of laboratory experiments to better understand wave-wave interaction processes that may control imbalanced solar wind turbulence at ion scales. Specifically, the project will investigate the behavior of two interactions between co-propagating Alfvén waves: a novel interaction driven by Hall physics, and the dispersive...
A HELIOGYRO SPACECRAFT IS A SPECIFIC TYPE OF SOLAR SAIL THAT GENERATES THRUST FROM THE REFLECTION OF SOLAR PHOTONS. THE PROPOSED RESEARCH FOR THIS FELLOWSHIP WILL ADDRESS THE LIMITATIONS OF CURRENT ANALYTIC MODELS AND CONTROL DESIGNS FOR A HELIOGYRO SPACECRAFT TO DEVELOP PRACTICAL SOLUTIONS. THE FIRST OBJECTIVE IS TO DERIVE NEW EQUATIONS OF MOTION FOR THE ESSENTIAL BLADE DYNAMICS. THE REDUCED ORDER MODEL FOR A HELIOGYRO SPACECRAFT WILL INCLUDE MULTIPLE DEGREES OF FREEDOM COUPLED DYNAMICS SOLAR RADIATION PRESSURE LOADING AND TORQUE SOURCE BOUNDARY CONDITIONS ALL OF WHICH ARE LACKING FROM THE CURRENT ANALYTIC MODELS. THE SECOND OBJECTIVE IS TO DEVELOP A ROOT CONTROL SYSTEM THAT EFFECTIVELY DAMPS THE STRUCTURAL MODES OF A HELIOGYRO SPACECRAFT. THE FINAL OBJECTIVE IS TO DETERMINE THE BLADE BEHAVIOR DURING INITIAL SPIN UP OF THE SPACECRAFT AND BLADE DEPLOYMENT. THE MAIN METHODS USED TO ACCOMPLISH THESE RESEARCH OBJECTIVES WILL INCLUDE CLASSICAL CONTROL THEORY IN CONJUNCTION WITH IMPEDANCE CONTROL AND A THOROUGH UNDERSTANDING OF THE BLADE DYNAMICS. THE HELIOGYRO SPACECRAFT MODELING WILL BEGIN WITH SIMPLIFIED LINEAR ASSUMPTIONS. THE COUPLING AND NONLINEARITIES WILL BE ADDED INCREMENTALLY TO THE MODEL. THE PROPELLANT FREE HELIOGYRO IS A LONG DURATION SUSTAINABLE SPACECRAFT WHOSE MANEUVERABILITY ALLOWS IT TO ATTAIN PREVIOUSLY INACCESSIBLE ORBITS FOR TRADITIONAL SPACECRAFT. CONTINUING RESEARCH IN PRACTICAL HELIOGYRO CONTROL WILL SIGNIFICANTLY ADVANCE THE TRL OF THIS INNOVATIVE DESIGN IN TURN LOWERING THE COST OF EXISTING MISSIONS AND OPENING UP EXCITING NEW MISSION POSSIBILITIES.
Mod # | Description | ReasonForModification | Federal Obligation | Date |
|---|---|---|---|---|
| Not listed | ($128) | 10/19/20 | ||
| 8 | Funding Only Action | ($128) | 10/19/20 | |
| Not listed | $35.0k | 7/19/19 | ||
| 7 | Funding Only Action | $35.0k | 7/19/19 | |
| Not listed | $0 | 7/14/19 |