Engineering
Thruster
100%
Electrospray
88%
Dielectrics
44%
Disinfection
33%
Flow Rate
19%
Atmospheric Pressure
17%
Corona Discharge
16%
Propulsion System
16%
Micro Propulsion
16%
Electric Field
15%
Duct
13%
Decontamination
13%
Applied Voltage
13%
Experimental Result
13%
Relative Humidity
12%
Specific Impulse
12%
Airflow Rate
11%
Response Characteristic
11%
Pressure Plasma
11%
Kinetic Model
11%
Humid Air
11%
Test Tube
11%
Advanced Space Propulsion Technology
11%
Direct Current
11%
Ignition
11%
Two Dimensional
11%
Rod
11%
Atmospheric Air
11%
Numerical Study
11%
Time-of-Flight
8%
Input Energy
8%
Fluid Model
7%
Carbon Nanotube
7%
Main Reason
5%
Thermostatics
5%
Consuming Process
5%
Performance Parameter
5%
Electrode Structure
5%
Plasma Reactor
5%
CubeSat
5%
Space Charge
5%
Material Science
Fourier Transform Infrared Spectroscopy
33%
Ionic Liquid
33%
Nucleic Acid
16%
Density
12%
CubeSat
11%
Electrospray
11%
Spectroscopy Technique
11%
Plasma Etching
11%
RNA
11%
Film
11%
Dielectric Material
11%
Dielectric Material
11%
Surface (Surface Science)
11%
Cathode
6%
Time-of-Flight Mass Spectrometry
5%
Biological Material
5%
Solvation
5%
Amino Acids
5%
Needle Electrode
5%
Machining
5%
Pore Size
5%
Physics
Dielectric Barrier Discharge
44%
Atmospheric Pressure
28%
Plasma Jet
22%
FTIR Spectroscopy
14%
Contours
11%
Biological Process
11%
Ionic Liquid
11%
Ion Propulsion
11%
Cold Plasma
7%
Cryogenic Temperature
7%
Air Flow
6%
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%
