Variable-Isp Ionic Liquid Electrospray Thruster

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,997.00
Award Year:
2009
Program:
STTR
Phase:
Phase I
Contract:
FA9550-09-C-0179
Award Id:
90199
Agency Tracking Number:
F08B-T09-0203
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
11 Tech Circle, Natick, MA, 01760
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
184629491
Principal Investigator:
Douglas Spence
Director, Micropropulsion
(508) 655-5565
doug@busek.com
Business Contact:
Judy Budny
Contracts Administrator
(508) 655-5565
judy@busek.com
Research Institute:
Massachusetts Institute of Tech.
Michael P Corcoran
77 Massachusetts Avenue
Cambridge, MA, 2139
(617) 253-3906
Domestic nonprofit research organization
Abstract
Busek proposes, with the MIT Space Propulsion Lab, to develop and characterize a variable-Isp colloid thruster operating only in the ionic mode and achieving its variable-Isp through use of a deceleration grid. This approach overcomes the usual inefficiencies encountered in variable-Isp colloid thruster operation, where lower Isp is accomplished through operation in droplet or mixed droplet/ion modes. An additional benefit is that the variable-Isp operation can be obtained under constant power. For the Phase 1 effort, the Busek/MIT team shall develop a linear emitter using photolithographic mask transfer and electrochemical etching on porous tungsten substrates. The emitter will subsequently be operated to determine V-I characteristics, verify ion emission and the decelerator concept, and perform time-of-flight measurements. Following these tests, direct thrust measurements shall be performed on Buseks magnetically levitated thrust stand to obtain direct thrust and Isp measurements. The linear emitter architecture will be designed in order to be suitable for multiplexing into thruster units able to provide greater thrust levels. Subsequent Phase 2 work would be to multiplex emitters and develop a deliverable 1mN class thruster with variable Isp of 500-5000 seconds. BENEFIT: Features of the proposed effort are: a colloid thruster able to operate only in ionic mode; variable Isp operation spanning 500-5000 seconds; and constant power operation. The benefit of pure ionic operation is that it avoids the inefficiencies of mixed-mode (droplet + ion) operation. Variable Isp provides versatility in a single thruster system, allowing for operations such as highly mass-efficient station-keeping as well as rapid maneuver that would otherwise require multiple systems. Constant power operation allows for simplification of power electronics design as well as reduced demands on the spacecraft bus, where variable power thrusters complicate power allocation and margin requirements.)

* information listed above is at the time of submission.

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