Design and fabrication of the thruster heads for the MicroThrust MEMS electrospray propulsion system
Design and fabrication of the thruster heads for the MicroThrust MEMS electrospray propulsion system
Microfabricated electrospray thrusters are widely acknowledged as one of
the most promising technologies for the propulsion of small spacecraft. Their relative simplicity, high efficiency (>70%), low footprint (M <500g, V <10cm3) and large potential specific impulse (>3000s) enable the creation of a miniature system capable of providing up to 5km/s∆ V to 3U CubeSats.
We report here on our latest efforts in the development of such a thruster system, completed within the MicroThrust (www.microthrust.eu) project. While a companion paper will present early test results of the thrusters, this paper will focus on their design and fabrication.
We use MEMS microfabrication to manufacture internally fed capillary emitters from silicon. This permits the high fluidic impedance required to get the necessary low flow rates associated with pure ionic mode operation, in addition to allowing the fabrication of large arrays of perfectly aligned, nearly identical emitters. We present for the first time the wafer-level integration of an acceleration stage, with individual electrodes operating on up to 127 emitters on a single chip. By adding the accelerator, we increase both the specific impulse and thrust generated by the emitters, while also increasing the thrust efficiency
by electrostatic focusing the spray.
We have fabricated chips with varying emitter density (213 and 125 emitters per
cm2) and have successfully tested passively fed emitter arrays, obtaining up to 35μA of current at +875V for a 91 emitter array
Dandavino, Simon
bf5b58c0-a6f3-4328-8cd5-00fb98f1b6ce
Ataman, Caglar
6b5eddda-d85a-498d-93b6-c4229472fc32
Chakraborty, Subha
2e16b493-c298-4952-8f2e-c55b57a64065
Shea, H.
c326ed63-07c2-408d-a809-1800fea5d7ec
Ryan, Charles
3627e47b-01b8-4ddb-b248-4243aad1f872
Stark, J.P.W.
8ceef3ee-a274-41bd-bfa7-29a06861510c
Dandavino, Simon
bf5b58c0-a6f3-4328-8cd5-00fb98f1b6ce
Ataman, Caglar
6b5eddda-d85a-498d-93b6-c4229472fc32
Chakraborty, Subha
2e16b493-c298-4952-8f2e-c55b57a64065
Shea, H.
c326ed63-07c2-408d-a809-1800fea5d7ec
Ryan, Charles
3627e47b-01b8-4ddb-b248-4243aad1f872
Stark, J.P.W.
8ceef3ee-a274-41bd-bfa7-29a06861510c
Dandavino, Simon, Ataman, Caglar, Chakraborty, Subha, Shea, H., Ryan, Charles and Stark, J.P.W.
(2013)
Design and fabrication of the thruster heads for the MicroThrust MEMS electrospray propulsion system.
33rd International Electric Propulsion Conference,, George Washington University, Washington, United States.
06 - 10 Oct 2013.
8 pp
.
(In Press)
Record type:
Conference or Workshop Item
(Paper)
Abstract
Microfabricated electrospray thrusters are widely acknowledged as one of
the most promising technologies for the propulsion of small spacecraft. Their relative simplicity, high efficiency (>70%), low footprint (M <500g, V <10cm3) and large potential specific impulse (>3000s) enable the creation of a miniature system capable of providing up to 5km/s∆ V to 3U CubeSats.
We report here on our latest efforts in the development of such a thruster system, completed within the MicroThrust (www.microthrust.eu) project. While a companion paper will present early test results of the thrusters, this paper will focus on their design and fabrication.
We use MEMS microfabrication to manufacture internally fed capillary emitters from silicon. This permits the high fluidic impedance required to get the necessary low flow rates associated with pure ionic mode operation, in addition to allowing the fabrication of large arrays of perfectly aligned, nearly identical emitters. We present for the first time the wafer-level integration of an acceleration stage, with individual electrodes operating on up to 127 emitters on a single chip. By adding the accelerator, we increase both the specific impulse and thrust generated by the emitters, while also increasing the thrust efficiency
by electrostatic focusing the spray.
We have fabricated chips with varying emitter density (213 and 125 emitters per
cm2) and have successfully tested passively fed emitter arrays, obtaining up to 35μA of current at +875V for a 91 emitter array
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Accepted/In Press date: 6 October 2013
Venue - Dates:
33rd International Electric Propulsion Conference,, George Washington University, Washington, United States, 2013-10-06 - 2013-10-10
Identifiers
Local EPrints ID: 449278
URI: http://eprints.soton.ac.uk/id/eprint/449278
PURE UUID: 73b3aaf6-0e34-465f-af22-da0018f0b65c
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Date deposited: 21 May 2021 16:31
Last modified: 16 Mar 2024 12:25
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Contributors
Author:
Simon Dandavino
Author:
Caglar Ataman
Author:
Subha Chakraborty
Author:
H. Shea
Author:
J.P.W. Stark
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