Engineering
Design
100%
Solar Thermal
100%
Thruster
87%
Receivers
50%
Optical Fiber
37%
Performance
37%
Miniaturization
37%
Satellites
37%
Models
25%
Design Process
25%
Solar Energy
25%
Orbital Transfer
25%
CubeSat
25%
Propulsion System
25%
Temperature
25%
Efficiency
12%
Thermal Model
12%
Heat Losses
12%
Inflatables
12%
Minimum Velocity
12%
Microelectromechanical System
12%
Attitude Control
12%
Thermal Energy
12%
Subsystems
12%
Water
12%
Standardization
12%
Nozzle
12%
Life Disposal
12%
Microchannel
12%
Research
12%
Final Design
12%
Concentrator
12%
Stored Energy
12%
Surface
12%
Operational Cost
12%
Transmissions
12%
Electric Propulsion
12%
Feasibility Study
12%
Integration
12%
Gas Fuel Manufacture
12%
Geometrical Parameter
12%
Specific Impulse
12%
Microscale
12%
INIS
design
100%
thermal analysis
100%
propulsion
88%
thrusters
77%
propellants
44%
miniaturization
33%
satellites
33%
optical fibers
33%
performance
33%
propulsion systems
22%
heat
22%
solar energy
22%
volume
22%
orbits
22%
surfaces
11%
manufacturing
11%
width
11%
power
11%
feasibility studies
11%
energy
11%
stored energy
11%
demand
11%
efficiency
11%
attitude control
11%
geometry
11%
range
11%
variations
11%
shape
11%
heat losses
11%
impulse
11%
operating cost
11%
inclination
11%
velocity
11%
nozzles
11%
throat
11%
water
11%
moon
11%
transmission
11%
concentrators
11%
microelectromechanical systems
11%
standardization
11%
iterative methods
11%
Keyphrases
Lunar Mission
100%
Intermediate Performance
14%
1U CubeSat
14%
Velocity Increment
14%
End-of-life Disposal
14%
Optical Fiber Bundle
14%
Nozzle Throat
14%
Low Lunar Orbit
14%