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More Efficient Electric Propulsion Via Reduced Mass of Xenon Propelant

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: N/A
Agency Tracking Number: 28340
Amount: $59,860.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Solicitation Year: N/A
Award Year: 1995
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
200 Yellow Place
Rockledge, FL 32955
United States
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Thomas Reinarts, Phd
 (407) 631-3550
Business Contact
Phone: () -
Research Institution

This Phase I project will determine the feasibility of developing a xenon propellant storage system for an electric propulsion engine that offers significant reductions in mass, volume, and storage pressure over the compressed vapor storage currently used. Electric propulsion systems utilizing xenon propellant provide a desirable alternative to other electric propulsion designs for orbital maintenance and transfer, due to higher efficiencies and thrust to power ratios. However, the current compressed storage pressure is 3000 psi, requiring high strength, high mass containers. Currently, the container is 15% of the combined xenon and container mass (for storage of 50 kg of xenon). Storage of xenon in the liquid or two-phase (liquid and vapor) state will reduce high pressure storage dangers by a factor of 20r system mass by as much as 16%, and storage volume by as much as 23%. Phase I of the research will design this system. Overall efficiency and performance of the electric propulsion unit will be improved. Preliminary Phase I testing will include a proof-of-concept demonstration. Phase II will include design optimization, construction, and testing of the lighter, smaller, safer storage system. The potential applications for this storage system are numerous. The use of xenon propellant in Hall thrusters and ion engines is fast becoming a competitive component of space exploration, station keeping and orbit transfers. The low pressure, low mass storage system proposed here will reduce costs and provide for the advancement of electric propulsion technologies in commercial and military.

* Information listed above is at the time of submission. *

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