SBIR/STTR Research Award

NanoFET - Nanoparticle Field Extraction Thruster for Micro-Satellites and Defensive Counterspace

Award identifier 7fa970cc855103f1e628b8a28ee7dba6d0e0ef915fbab09fdc5e1ca5176e9a3aAwarding agency Department of Defense · Air Force

Award amount

$499,917

Program and phase

STTR · Phase II

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Electrodynamic Applications Inc
Proposal award date
2008-11-20
Contract end date
2010-11-20
UEI
EKN4D4FDZNV9
Solicitation number
Not reported
Topic code
AF07-T036

Research abstract

The Nanoparticle Field Extraction Thruster (NanoFET) is being developed as a high thrust-to-power, highly compact, variable specific impulse electric propulsion device especially for micro-satellite applications. NanoFET provides thrust by extracting and charging nanometer to micron-sized conducting particles (e.g., spheres) fed from a dry reservoir and accelerating them electrostatically. This technique may allow important advantages in terms of storage and handling efficiency over gas or liquid propellant approaches. The particles are delivered from the reservoir spring force and piezoelectric vibrations. Charging and extraction is done using a multi-layer MEMS grid. By charging equal numbers of particles both positively and negatively, NanoFET can eliminate the need for a neutralizer. Highly efficient in terms of both power and system mass/volume, NanoFET could provide significant improvement over current propulsion options for key micro-satellite mission applications. Current design targets are tens of nanometer particles accelerated through tens of kilovolts. Prototype experiments have been conducted with 5-micron hollow aluminum spheres as an interim step. In addition to propulsion, the particle beam created by NanoFET provides capability for defensive counter-space applications including sensor coating and momentum transfer interactions with non-friendly spacecraft. Potential mission applications include deployable "Sentinel" sub-satellites that would provide mother-satellite inspection or proximate satellite interception. BENEFIT: The NanoFET propulsion system may find particular value in microsatellites attached to high value military assets. Small deployable spacecraft could thus provide mothercraft inspection, sentinel-like protection, plus other capabilities of value. The NanoFET propulsion system will also support other propulsion applications beyond military satellites. As a scalable technology, NanoFET could provide its variable thrust and Isp benefits to a wide range of civilian and research satellites in many size categories. In addition, the work being done to characterize the material impact of the NanoFET system in application to defensive counter space will benefit the development of versions of NanoFET for terrestrial applications. For example, in material processing it can be used to implant materials in accurately controlled quantities to specific depths and precise locations. We are presently working with UM to acquire funding to develop print applications through the MUCI university research grant program. Ultimately, we see potential for medical applications as well. EDA plans to develop and grow this technology into all of these areas.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

29 SBIR/STTR records share this UEI (2003–2015). Reported award amounts total $7,439,985. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, National Science Foundation

Agency intelligence

Department of Defense

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