Mueller, Ziemer, Hofer, Wirz, O’Donnell 15
Survey of Micro-Thrust Propulsion Options
Cube Sat - 5’th Annual Developers Workshop 2008
Micro-fabricated Colloid and FEEP
Fuel Tank
Manifold
Spout
Channel
Clip
system
Fuel Inlet
Description:
•
Micromachined versions of colloid thruster technology.
•
Micromachining allows for the precise fabrication of a much
greater number of emitters than in conventional approaches.
•
Since emitter tips are on micron-scale for conventional architectures,
increased number of emitter tips may result in increased thrust levels
at smaller device mass and volume for micromachined devices.
Status:
•
Laboratory development -
feasibility studies.
•
Micro-colloid/FEEP work past and ongoing at MIT (in collaboration Yale
U,
Busek Corp.), Almeda Applied Sciences (AASC), JPL, SRI International,
Sandia, U. Southampton/UK, Kings College/UK.
•TRL ~2-3.
Key Technology Characteristics:
•
Application: Constellation control, even of large constellation craft,
attitude control, small delta-v of micro/nanosats (constellations).
•
Very high precision thrust and impulse bits.
•
Widely scalable thrust levels by adjusting number of emission sites
per chip.
•
Relatively high thrust-to-power for electrostatic devices (colloids, not FEEPs).
•
Compact propellant storage.
•
Low TRL -
requires substantial development.
•
Neutralizer development, contamination studies, etc. required as
for
larger scale devices.
MIT Micro-Colloid Concept
JPL Micro-Colloid Test Fabrication Articles
Comments to this Manuals