Study
Prototype Liquid propellant pulsed plasma thruster
Liquid propellant impingement in an injector
Laser profile for throttleable solid propellant microthruster
Electric propulsion
Liquid propellant pulsed plasma thruster (LP-PPT)
Arcjet thruster using dimethyl ether (DME) as propellant
Pulsed plasma thruster using dimethyl ether (DME) as propellant
Magneto Plasma Dynamics (MPD) thruster
Anode layer type Hall thruster
Chemical/electric dual mode thruster using microwave
Arcjet firing
Chemical propulsion
Throttleable solid propellant microthruster using laser-assisted combustion
Combustion control using electric discharge
Bipropellant microthruster using nitrous oxide and dimethyl ether
Liquid propellant thruster using arc-discharge assisted combustion
Hybrid thruster for spacecraft
Heat flux evaluation for burning solid propellant by use of thermography and laser heating
Chemical/electric dual mode thruster using microwave
Solid propellant microthruster firing