| Outline |
Indent Level
| |
| Color | Curly Brackets (indicating CPC extensions to IPC) | |
CPC | COOPERATIVE PATENT CLASSIFICATION | ||
![]() | PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR (from combustion products F02K) |
![]() | Using plasma to produce a reactive propulsive thrust (generating plasma H05H 1/00) { (ion sources per se H01J 27/02, ion sources for plasma processing or ion beams H01J 37/08)} |
![]() | F03H 1/0006 | . | { Details applicable to different types of plasma thrusters (arrangements specially adapted for fitting plasma engines in or to cosmonautic vehicles B64G 1/405)} |
F03H 1/0012 | . . | { Means for supplying the propellant} |
F03H 1/0018 | . . |
F03H 1/0025 | . . | { Neutralisers, i.e. means for keeping electrical neutrality} |
F03H 1/0031 | . . | { Thermal management, heating or cooling parts of the thruster (temperature control for cosmonautic vehicles B64G 1/50)} |
![]() | F03H 1/0037 | . | { Electrostatic ion thrusters} |
F03H 1/0043 | . . |
F03H 1/005 | . . | { using field emission, e.g. Field Emission Electric Propulsion [FEEP} ] |
F03H 1/0056 | . . | { with an acceleration grid and an applied magnetic field} |
![]() | F03H 1/0062 | . . | { grid-less with an applied magnetic field} |
F03H 1/0081 | . | { Electromagnetic plasma thrusters} |
F03H 1/0087 | . | { Electro-dynamic thrusters, e.g. pulsed plasma thrusters} |
F03H 1/0093 | . | { Electro-thermal plasma thrusters, i.e. thrusters heating the particles in a plasma (resistojets per se B64G 1/406)} |
F03H 3/00 | Use of photons to produce a reactive propulsive thrust |
F03H 99/00 | Subject matter not provided for in other groups of this subclass |