Helicon Hall Thruster

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,997.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
FA9300-05-M-3008
Agency Tracking Number:
F051-204-3148
Solicitation Year:
2005
Solicitation Topic Code:
AF05-204
Solicitation Number:
2005.1
Small Business Information
ELECTRODYNAMIC APPLICATIONS, INC.
P.O. Box 131460, Ann Arbor, MI, 48113
Hubzone Owned:
N
Socially and Economically Disadvantaged:
Y
Woman Owned:
N
Duns:
610511334
Principal Investigator:
David Morris
Senior Engineer
(734) 786-1434
morris@edapplications.com
Business Contact:
David Morris
Senior Engineers
(734) 786-1434
morris@edapplications.com
Research Institution:
n/a
Abstract
The Hall thruster has great potential in satisfying many of the spacecraft propulsion needs of the United States Air Force for the next several decades due to its combination of high specific impulse, high thrust efficiency, and high thrust density. The USAF has recently concluded that bi-modal Hall thrusters (i.e., high thrust-to-power and high specific impulse) are attractive for future missions such as LEO-to-GEO orbital transfer vehicles (OTVs). To that end, the USAF has recently issued a contract to an Aerojet-led team to develop a 20-kW xenon-propellant Hall thruster that adheres to IHPRPT Phase III goals. Our proposal seeks to develop a new, two-stage Hall thruster that can achieve IHPRPT Phase III goals by using a helicon ionization, first-stage coupled to a state-of-the-art Hall accelerator stage. Use of the helicon ionization source, which is one of the world's most efficient, will allow high Hall thruster efficiency at low discharge voltages by reducing the ion production cost. Moreover, given the helicon source affinity for noble gases, it may be possible to develop an efficient Hall thruster that operates with propellants that are cheaper than xenon, such as argon.

* information listed above is at the time of submission.

Agency Micro-sites

US Flag An Official Website of the United States Government