SEDSAT-2 SWOT analysis of uppt vrs magnetics

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SEDSAT-2 Main Page


SEDSAT-2 ADCS

Contents

Magnetic System

Determination: Magnetometers

Control: Magnetic Coils

Detailed documentation: http://www.cubesat.auc.dk/, http://www.ncube.no/

SWOT Analysis

Strenghts Weaknesses
> Often used by other CubeSats (well tested)
> cheap
> no moving parts
> interaction with magnetometers
> not innovative
> not free
Opportunities Threats
> None > None


Micro propulsion system

µPPT

see http://en.wikipedia.org/wiki/Pulsed_plasma_thruster for general information

Design Goals for µPPT by ARC Seibersdorf (we would get fly-ready prototypes for SEDSat):

- Impulse bit: 10-20µNs, which would guarantee a pointing accuracy of <1 degree
- Spec. impulse: 500-1000 s
- Power: 0,5-1,5 W
- Weight: < 30g

SWOT Analysis

Strenghts Weaknesses
> Innovative (I think the first use with CubSat)
> Very Accurate (<1°)
> Electr. Prop: Can almost never run out of propellant
> non-toxic propellant (Teflon)
> professional manufactured devices
> free
> High electr. Power Consumption (maybe up to 1,5 W per Thruster)
> relatively heavy (<30g) -> only 6 thruster configuration to use
Opportunities Threats
> Could also be used for Orbit Changes (in limits), with additional thruster(s)
> PR for using an innovative new technology for CubeSat
> Not available before Fall 2008
> New Technology (first ones to test)
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