SBIR/STTR Research Award
Innovative High Energy Density Storage in Nano Vacuum Tubes (NVTs) Designed for Small Leakage Curren
Award amount
$125,000Program and phase
STTR · Phase IAward year
2016Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- APPLIED MATERIAL SYSTEMS ENGINEERING, INC
- Proposal award date
- 2016-06-10
- Contract end date
- 2017-06-09
- UEI
- HEW9FKHKU6F8
- Solicitation number
- Not reported
- Topic code
- T3.02
Research abstract
NASA's various Space Mission Directorate seek to develop technology to fulfill the technology gap and to enable missions with the unique high energy density charge storage technology. The overall goal of this STTR proposal is attempt to develop the novel energy storage technology to enable and enhance the capabilities of future NASA missions. The unique set of requirements for the power systems for various missions have emerged and they vary greatly, with advancements in components needed above the current State of the Art for high energy density, high power density, long life, high reliability, low mass/volume, radiation tolerance, and the wide temperature operation. For this STTR our first goal is evaluation of the concept of Nano Vacuum Tube (NVT) based charge storage device design that can provide High Energy Density storage with significant mass savings. The feasibility evaluation of design approaches are suggested to meet the desired special needs of charge storage in space. As a second goal, it plans to leverage IR&D done at UIUC and AMSENG to bring together unique experience base team to undertake the feasibility study to fulfill the identified technology gap through prototype development. Although the theory developed at UIUC predicts that storage of GJ/m3 charges is feasible in Nano Vacuum Tubes, the proposed experiments will decide what is feasible and which design options delivers the performance in space, when one uses the space stable heritage light weight materials. Finally, the suggested material designs and the devices need to meet reliability needs of the space mission environment for a typical ten year mission lifetime and conform to the mission space qualification needs and the requirements including high vacuum, microgravity, radiation, atomic oxygen, low out gassing, and high launch loads. The phase I - feasibility evaluation and the phase II - validation efforts suggested herewith can help us to fulfill the technology gap
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Innovative Advances in Coatings for Extreme Environmental Thermal Radiators and Complex Surfaces
- Advanced Affordable Technologies For Nuclear Applications
- Integration of Dust Resisting Secondary Emission Engineered Passive Thermal Control Material Systems (TCMS) Coating on - Flight & Test Hardware and Its Performance Validation Testing Per NASA-STD-1008
- Novel Coating Concepts for Lunar Regolith Dust Mitigation for Thermal Radiators and Extreme Environments
- Advanced Survivable Thermal Control Material Systems for Aggressive Planetary Dusty Environments