Field Emission Cathode for Electrodynamic Tethers

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$69,961.00
Award Year:
2002
Program:
SBIR
Phase:
Phase I
Contract:
NAS8-01151
Agency Tracking Number:
012988
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Busek Co. Inc.
11 Tech Circle, Natick, MA, 01760
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Vlad Hruby
President
(508) 655-5565
vhruby@busek.com
Business Contact:
Judy Budny
Business Official
(508) 655-5565
judy@busek.com
Research Institution:
n/a
Abstract
Electrodynamic (ED) tethers offer the potential of propellant-less propulsion with infinite specific impulse (Isp). To achieve it, an efficient electron source that contacts the space plasma without using propellant must be coupled with the ED tether. At present, the electrons are supplied by a hollow cathode (HC) plasma contactor with complex propellant management and storage and power-processing unit that typically dominate the ED tether system mass. Busek therefore proposes the development of a field emission electron source that uses no propellant, and is less massive and less complex than the HC system.In Phase I we will design, build, and test a field emission array cathode (FEAC) using Busek-grown carbon nanotubes as the emitters. The FEAC will consist of four paralleled emitter cells that will be tested individually and as a combined FEAC panel. The cell technology was already demonstrated as a neutralizer on a laboratory colloid thruster. Scaling up this technology while maintaining adequate current density is the major Phase I challenge.In Phase II, a complete FEAC panel system consisting of many cells will be developed per typical ED tether requirements. The system will include the FEAC power-processing unit and emission control circuitry for autonomous tether current matching.

* information listed above is at the time of submission.

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