Control Valve for Miniature Xenon Ion Thruster

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNC08CA39C
Agency Tracking Number: 066747
Amount: $599,883.00
Phase: Phase II
Program: SBIR
Awards Year: 2008
Solitcitation Year: 2006
Solitcitation Topic Code: S3.01
Solitcitation Number: N/A
Small Business Information
Mide Technology Corporation
200 Boston Avenue, Suite 1000, Medford, MA, 02155-4243
Duns: 78612
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Attila Lengyel
 Principal Investigator
 (781) 306-0609
Business Contact
 Petra Botha
Title: Business Official
Phone: (781) 306-0609
Research Institution
NASA is continuing its development of electric propulsion engines for various applications. Efforts have been directed toward both large and small thrusters, depending on the end use. A current program is focused on the development of a miniature thruster. Development of a Miniature Xenon Ion (MiXI) thruster will enable precision spacecraft positioning and formation maneuvers for formation-flying spacecraft. The current MiXI thruster prototype will provide 0.5 – 3 mN thrust at 3000 sec specific impulse and efficiencies around 50% or better. The MiXI thruster will use Xenon propellant, a noble gas, minimizing spacecraft contamination.( One of the challenges of such a thruster is to be able to accurately control the flow of propellant. The required flow rates are on the order of 0.1 to 1.0 sccm of Xenon. To this end Midé, in Phase I, demonstrated that a small flow control valve, based on piezoelectric technology, met all performance objectives. Midé is a world leader in this technology, demonstrated by its existing patented packaged actuator product line and past valve experience. Aerojet provided electric propulsion expertise for the duration of the program and serve as a technology integration and transition path.

* information listed above is at the time of submission.

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