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Bifunctional Membrane for High Energy, Long Shelf Life Li-S Batteries, Phase I
The adoption of high energy lithium sulfur batteries hinges on significant improvements in charge/recharge cycle life. Cycle life is limited by migration of dissolved... -
Thermoacoustic Duplex Technology for Cooling and Powering a Venus Lander, Pha...
Sierra Lobo proposes to develop a technology that can provide both cooling and electric power generation using heat. When coupled with a radioisotope heat source, the... -
Multifunctional Aerogel Thermal Protection Systems for Hypersonic Vehicles, P...
The overall objective of the Phase II project is to develop lightweight reinforced aerogel materials for use as the core structural insulation material in multifunctional... -
In-Situ Resource Utilization: Oxygen Production
The leading option for extracting oxygen from the Mars atmospheric carbon dioxide is to use a solid oxide electrolyzer, which removes one oxygen atom from the CO2 molecule,... -
Pistonless Pumps for Nanosat Launch and Sample Return Vehicles, Phase I
This proposal responds to the request for pumps for pressure-fed propulsion systems with a pistonless pump wherein a pressurant act directly on the propellant(s) in a set of... -
HIGH PERFORMANCE CARBON NANOTUBE BASED CONDUCTORS, Phase I
This proposal is for the development of conductors with improved electrical conductivity and/or ampacity better than copper or aluminum. Electrical conductors are key... -
Mobile Passive MWIR Gas Imager, Phase I
In this SBIR project Boston Applied Technologies, Inc. (BATi) proposes a unique optical imager for remote gas sensing. Tunable filters based on electro-optic effect have shown... -
Microwave Radiometer for Aviation Safety, Phase I
SBIR Phase I Project proposes a new passive microwave airborne sensor for in flight icing hazard detection, Microwave Radiometer for Aviation Safety. A feasibility study of a... -
Multi-Purpose Interplanetary Deployable Aerocapture System (MIDAS), Phase I
Altius Space Machines and MSNW LLC propose the development of a cubesat-scale Multipurpose Interplanetary Deployable Aerocapture System (MIDAS), to provide cubesats with the... -
High Radiation Tolerant Ceramic Voltage Isolator (Non-optical Gate Driver), P...
The goal of the Phase I effort is to design, develop and demonstrate a novel solid-state ceramic-based voltage isolator and demonstrate its potential to provide a highly... -
Bi2212 Superconductors for High-Power Density Motors for Aero Propulsion, Pha...
Future hybrid aircraft, such as NASA’s N3-X plan, will require all-superconducting electric motors and generators in order to achieve power density in excess of 10 kW/kg.... -
Innovative Health Monitoring Techniques for High Temperature Composites
High temperature composite materials, which include ceramic matrix composites (CMCs), carbon-carbon and polyimide composites, will be essential for future space vehicles that... -
Energetic Materials For Advanced Volume Limited Propulsion Systems Applicatio...
Energetic Materials For Advanced Volume Limited Propulsion Systems Applications, Phase I -
Green Monopropellant Microtube Combustor for CubeSat Propulsion
This project developed an alternate structure and alloy to serve as a green monopropellant catalyst. This innovation, a catalytic microtube thruster, is an original design... -
Wideband Autonomous Cognitive Radios for Networked Satellites Communications,...
Wideband Autonomous Cognitive Radios (WACRs) are advanced radios that have the ability to sense state of the RF spectrum and the network and self-optimize its operating mode in... -
Hybrid Electric Propulsion System for a VTOL/Multirotor Aircraft, Phase II
LaunchPoint Technologies proposes to build a scalable hybrid electric propulsion system. LaunchPoint will build and fly a 1 kW hybrid electric vehicle and will build and bench... -
Liquid Sorption Pump, Phase I
The Liquid Sorption Pump (LSP) is a new technology for acquiring CO2 from the Martian atmosphere for use in In Situ Resource Utilization (ISRU) systems. In the LSP, propanol is... -
Green Monopropellant Secondary Payload Propulsion System, Phase I
In recent work for the Air Force, Ultramet demonstrated nearly one thousand restarts with repeatable pulse performance and steady-state burn characteristics using AF-M315E... -
A Quantum Cascade Laser-Based CO Sensor for Fire Warning, Phase I
Maxion Technologies and Physical Sciences Inc. (PSI) propose to jointly develop a compact, rugged, highly reliable, and autonomous sensor for in-situ monitoring of CO in... -
An Ultra-Sensitive, Size Resolved Particle Mass Measurement Device, Phase I
The characterization of aircraft particulate matter (PM) emissions has benefited greatly by the Aerosol Mass Spectrometer (AMS) by providing size resolved compositional...