NASA SBIR 01-II Solicitation

FORM 9B - PROPOSAL SUMMARY


PROPOSAL NUMBER: S3.02-9233 (For NASA Use Only - Chron: 012766 )
PHASE-I CONTRACT: NAS3-02048
PROPOSAL TITLE: Capillarity Driven Flow Of Propellant Liquids In Colloidal Satellite Thrusters

TECHNICAL ABSTRACT (LIMIT 200 WORDS)
The objective of this project is to develop colloidal thrusters capable of producing the thrust levels required to overcome drift and maintain individual microsatellites at their assigned positions.
In the Phase I research on this project, we showed that the use of capillarity driven flow of non-volatile propellant liquid through a porous matrix or "wick" could produce extremely stable electrosprays in vacuum of charged droplets. Inherent in this use of "wick" injection is that the flow rate of propellant liquid, and thus the thrust level for a particular thruster, is determined entirely by the applied voltage without any need for additional flow rate control circuitry. Moreover, this inherent simplicity, relative to other colloidal propulsion systems, means that multiplexing of such wick injectors is simple and straight-forward so that any desired level of thrust over a wide range can be achieved simply by varying the number of these simple wick thrusters.
The objective of the proposed Phase II research is to implement the results of our Phase I research by designing, constructing and testing prototype wick thrusters with both conventional needle designs and to investigate similar applications using MEMS technology.

POTENTIAL COMMERCIAL APPLICATIONS
Electrospray feed by capillarity driven flow provides an improved means of colloidal satellite propulsion yielding increased reliabilty, efficiency, and reduced weight over competitive systems employing hydrostatic feed mechanisms. Commercial applications include not only users of colloidal satellite thrusters, but numerous biomedical applications of electrospray mass spectrometry, where small sources are often plagued by plugging as a result of dirt or particulate media. Stable sprays for both ES-MS and Colloidal thrusters can be achieved simply by adjusting the applied electrostatic field.

NAME AND ADDRESS OF PRINCIPAL INVESTIGATOR (Name, Organization Name, Mail Address, City/State/Zip)
Joseph Bango
Connecticut Analytical Corporation
696 Amity Road
Bethany , CT   06524 - 3006

NAME AND ADDRESS OF OFFEROR (Firm Name, Mail Address, City/State/Zip)
Connecticut Analytical Corporation
696 Amity Road
Bethany , CT   06524 - 3006


Form Printed on 05-09-02 16:37