Jackson, 2017 - Google Patents
Design of an air-breathing electric thruster for CubeSat applicationsJackson, 2017
View HTML- Document ID
- 6635468578779196532
- Author
- Jackson S
- Publication year
External Links
Snippet
The altitude range between 120 and 300 km is relatively unexplored with regard to space weather, atmospheric models, climate observations, the global electric circuit, remote sensing, and intelligence gathering. This altitude range is not conducive to to in situ …
- 239000002245 particle 0 abstract description 152
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS; PRODUCING MECHANICAL POWER; OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0006—Details applicable to different types of plasma thrusters
- F03H1/0012—Means for supplying the propellant
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Zheng et al. | A Comprehensive Review of Atmosphere‐Breathing Electric Propulsion Systems | |
| Jackson | Design of an air-breathing electric thruster for CubeSat applications | |
| Garrigues et al. | Electric propulsion: comparisons between different concepts | |
| Singh et al. | A review of research in low earth orbit propellant collection | |
| Garrigues | Computational study of hall-effect thruster with ambient atmospheric gas as propellant | |
| Bamford et al. | An exploration of the effectiveness of artificial mini-magnetospheres as a potential solar storm shelter for long term human space missions | |
| Sheehan et al. | Initial Operation of the CubeSat Ambipolar Thruster | |
| US12188456B2 (en) | Plasma engine with leptonic energy source | |
| Herdrich et al. | Advanced plasma (propulsion) concepts at IRS | |
| Zheng et al. | Design and Optimization of vacuum Intake for Atmosphere-Breathing electric propulsion (ABEP) system | |
| Fan et al. | Discharge characteristics of Hall thruster with large height-radius ratio | |
| Matyash et al. | Kinetic simulations of SPT and HEMP thrusters including the near-field plume region | |
| Gomez et al. | Modelling an Ion Thruster for a Small Spacecraft in Very Low Earth Orbit | |
| Yavuz et al. | Prototype design and manufacturing method of an 8 cm diameter RF ion thruster | |
| Lyons et al. | Electric propulsion concepts enabled by high power systems for space exploration | |
| Feng | Investigation of a Novel Atmosphere-Breathing Electric Propulsion Platform and Intake | |
| Karimov et al. | The use of interplanetary medium as fuel for plasma thrusters | |
| Chan-Ying et al. | Simulation and design of a micro-hall thruster for spacecraft | |
| Dannenmayer et al. | Elementary scaling laws for sizing up and down Hall effect thrusters: Impact of simplifying assumptions | |
| Chiba et al. | Characterization of helicon plasma thruster performance operated for various rare gas propellants | |
| Kozhevnikov et al. | Development of the Radio-Frequency Ion Thruster on Atmospheric Gases | |
| Turchi | An electric propulsion memoir | |
| LaPointe | High power theta-pinch propulsion for piloted deep space exploration | |
| Shen et al. | Development of a micro ECR ion thruster for space propulsion | |
| Frischauf et al. | MOA2—an R&D paradigm buster enabling space propulsion by commercial applications |