Engineering
Thruster
100%
Electrospray
90%
Dielectrics
50%
Disinfection
40%
Flow Rate
17%
Atmospheric Pressure
15%
Applied Voltage
15%
Corona Discharge
15%
Propulsion System
15%
Micro Propulsion
15%
Electric Field
14%
Influencing Factor
13%
Specific Impulse
13%
Duct
12%
Decontamination
12%
Experimental Result
11%
Relative Humidity
11%
Discharge Mode
11%
Airflow Rate
10%
Response Characteristic
10%
Pressure Plasma
10%
Kinetic Model
10%
Humid Air
10%
Test Tube
10%
Advanced Space Propulsion Technology
10%
Direct Current
10%
Ignition
10%
Two Dimensional
10%
Rod
10%
Atmospheric Air
10%
Numerical Study
10%
Time-of-Flight
8%
Input Energy
7%
Fluid Model
6%
Carbon Nanotube
6%
Main Reason
5%
Thermostatics
5%
Consuming Process
5%
Performance Parameter
5%
Electrode Structure
5%
Plasma Reactor
5%
CubeSat
5%
Space Charge
5%
Material Science
Ionic Liquid
40%
Fourier Transform Infrared Spectroscopy
30%
Nucleic Acid
15%
Density
11%
CubeSat
10%
Electrospray
10%
Spectroscopy Technique
10%
Plasma Etching
10%
RNA
10%
Film
10%
Dielectric Material
10%
Dielectric Material
10%
Surface (Surface Science)
10%
Machining
8%
Cathode
6%
Time-of-Flight Mass Spectrometry
5%
Biological Material
5%
Solvation
5%
Amino Acids
5%
Needle Electrode
5%
Pore Size
5%
Physics
Dielectric Barrier Discharge
40%
Atmospheric Pressure
25%
Plasma Jet
20%
FTIR Spectroscopy
13%
Contours
10%
Biological Process
10%
Ionic Liquid
10%
Ion Propulsion
10%
Cold Plasma
6%
Cryogenic Temperature
6%
Air Flow
5%
Electric Fields
5%
Charged Particle
5%
Amino Acid
5%
Infrared Spectra
5%
Nucleic Acid
5%
Phospholipid
5%
Thermal Plasma
5%
Solvation
5%
Spacecraft Control
5%
