Delta 50-820 User Manual Page 18

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Mueller, Ziemer, Hofer, Wirz, O’Donnell 18
Survey of Micro-Thrust Propulsion Options
Cube Sat - 5’th Annual Developers Workshop 2008
Electric Propulsion: Precision attitude control or high-Isp
delta-V
Miniature Ion Propulsion (MiXI):
JPL developed miniature ion engine technology may satisfy Cube sat design envelope for multi-
cube (3-cube “brick”, 6 cube “six pack”) architectures with deployable arrays.
Power limitations may require MiXI
to be operated in throttle mode at limited thrust, however, at
T/W ratios not unlike on larger EP propelled spacecraft.
Vacuum Arc Thruster:
Developed by Almeda
Applied Sciences for micro-
and formation flying control
Cube sat architectures have already been explored (single cube).
Primarily suited for attitude control due to inherently pulsed operation and low total impulse.
Pulse Plasma Thrusters:
Smaller PPT versions have been developed for micro-sat application (Dawgstar).
Primarily suited for attitude control due to inherently pulsed operation and low total impulse.
Summary of Propulsion Candidates
for CubeSats
-
cont’d
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