INIS
attitude control
11%
concentrators
11%
demand
11%
design
100%
efficiency
11%
energy
11%
feasibility studies
11%
geometry
11%
heat
22%
heat losses
11%
impulse
11%
inclination
11%
iterative methods
11%
manufacturing
11%
microelectromechanical systems
11%
miniaturization
33%
moon
11%
nozzles
11%
operating cost
11%
optical fibers
33%
orbits
22%
performance
33%
power
11%
propellants
44%
propulsion
88%
propulsion systems
22%
range
11%
satellites
33%
shape
11%
solar energy
22%
standardization
11%
stored energy
11%
surfaces
11%
thermal analysis
100%
throat
11%
thrusters
77%
transmission
11%
variations
11%
velocity
11%
volume
22%
water
11%
width
11%
Engineering
Attitude Control
12%
CubeSat
25%
Design
100%
Design Process
25%
Determines
12%
Electric Propulsion
12%
Feasibility Study
12%
Final Design
12%
Gas Fuel Manufacture
12%
Geometrical Parameter
12%
Heat Losses
12%
Inflatables
12%
Life Disposal
12%
Microelectromechanical System
12%
Microscale
12%
Miniaturization
37%
Minimum Velocity
12%
Models
25%
Nozzle
12%
Operational Cost
12%
Orbital Transfer
25%
Propulsion System
25%
Receivers
50%
Satellites
37%
Solar Energy
25%
Solar Thermal
100%
Specific Impulse
12%
Stored Energy
12%
Subsystems
12%
Thermal Energy
12%
Thermal Model
12%
Thruster
87%
Transmissions
12%