INIS
design
100%
wheels
100%
testing
100%
satellites
100%
power
55%
control
33%
space
33%
performance
33%
stabilization
22%
flywheels
22%
attitude control
22%
speed
22%
cost
22%
miniaturization
11%
levels
11%
units
11%
applications
11%
universities
11%
range
11%
torque
11%
attitudes
11%
compacts
11%
storage
11%
volume
11%
motors
11%
form factors
11%
buses
11%
data
11%
steady-state conditions
11%
size
11%
electric motors
11%
balances
11%
orbits
11%
Engineering
Small Satellite
100%
Assembly
100%
Design
100%
Electric Power Utilization
75%
Models
50%
Picosatellites
50%
Demonstrates
50%
Attitude Control
50%
Flywheel
50%
Earth Observation
25%
Functional Performance
25%
Subsystems
25%
Drives
25%
Low Earth Orbit
25%
Full Speed
25%
Miniaturization
25%
Power Requirement
25%
High Data Rate
25%
Term Performance
25%