Leifer et al., 1992 - Google Patents
Electrostatic propulsion using C60 moleculesLeifer et al., 1992
- Document ID
- 11932901692261245252
- Author
- Leifer S
- Rapp D
- Saunders W
- Publication year
- Publication venue
- Journal of Propulsion and Power
External Links
Snippet
BUCKMINSTERFULLERENE, a newly discovered al-lotrope of carbon (C60), K2 has demonstrated properties that make it an excellent candidate propellant for electrostatic propulsion. Here, a discussion is presented of the potential benefits C60 ion propulsion may …
- 150000002500 ions 0 abstract description 52
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Nishiyama | Air breathing ion engine concept | |
| Garrigues | Computational study of hall-effect thruster with ambient atmospheric gas as propellant | |
| US5239820A (en) | Electric propulsion using C60 molecules | |
| Ferrato et al. | Rarefied flow simulation of conical intake and plasma thruster for very low earth orbit spaceflight | |
| Leifer et al. | Electrostatic propulsion using C60 molecules | |
| Patterson et al. | Low-power ion propulsion for small spacecraft | |
| Reader | Scale effects on ion rocket performance | |
| Koda et al. | Characteristics of ion–ion thruster generating continuously positive and negative ion beams | |
| US9334856B2 (en) | System and method of photoionization of fullerene and derivative clusters for high thrust-density ion thrusters | |
| Reader et al. | A submillipound mercury electron bombardment thruster | |
| Komurasaki | An overview of electric propulsion activities in Japan | |
| Grigoryan | Ion sources for space thrusters | |
| Shemansky | The role of solar wind heavy ions in the space environment51 | |
| Saunders | Stephanie D. Leifer* Jet Propulsion Laboratory | |
| Xinwei et al. | Experimental and numerical simulation study of the effect for the anode positions on the discharge characteristics of 300 W class low power Hall thrusters | |
| Suttrop | Comment on'Experimental study on autoignition in a scramjet combustor' | |
| BERKOPEC et al. | NASA electric propulsion technology | |
| Kaufman | Charge-exchange plasma generated by an ion thruster | |
| Patterson et al. | Derated ion thruster design issues | |
| SUTHERLAND | Recent advances in space propulsion | |
| Kammash et al. | Reaction physics and mission capabilities of the magnetically insulated inertial confinement fusion reactor | |
| MALOY et al. | Electric propulsion-Characteristics, applications, and status | |
| Hively | Preliminary design of a demonstrational ion rocket engine | |
| Cox | Condensation Colloid Propellants for Electrostatic Propulsion | |
| Parker et al. | iSat Surface Charging and Thruster Plume Interactions Analysis |