SERT II - Durability of the hollow cathode and future applications of hollow cathodes

Autor:	V. K. Rawlin, W. R. Kerslake
Rok vydání:	1970
Předmět:	Propellant Engineering System development Spacecraft propulsion Spacecraft Ion thruster business.industry Electrical engineering Aerospace Engineering Cathode Life testing law.invention Electrically powered spacecraft propulsion Space and Planetary Science law Aerospace engineering business
Zdroj:	Journal of Spacecraft and Rockets. 7:14-20
ISSN:	1533-6794 0022-4650
DOI:	10.2514/3.29856
Popis:	1 Kerslake, W. R., Byers, D. C., and Staggs, J. F., "SERT II Experimental Thruster System," AIAA Paper 67-700, Colorado Springs, Colo., 1967; also "SERT II: Mission and Experiments," Journal of Spacecraft and Rockets, Vol. 7, No. 1, Jan. 1970, pp. 4-6. 2 Kerrisk, D. J. and Kaufman, H. R., "Electric Propulsion Systems for Primary Spacecraft Propulsion," AIAA Paper 67-424, Washington, D. C., 1967. 3 Bechtel, R. T., "Discharge Chamber Optimization of the SERT II Thruster," Journal of Spacecraft and Rockets, Vol. 5, No. 7, July 1968, pp. 795-800. 4 Bechtel, R. T., Csiky, G. A., and Byers, D. C., "Performance of a 15-Centimeter Diameter, Hollow-Cathode Kaufman Thruster," AIAA Paper 68-88, New York, 1968. 5 Sohl, G., Speiser, R. C., and Wolters, J. A., "Life Testing of Electron-Bombardment Cesium Ion Engines," AIAA Paper 66233, San Diego, Calif., 1966. 6 Sellen, J. M. and Kemp, R. F., "Research on Ion Beam Diagnostics," TRW-4381-6017-RO-000, NASA CR-54692, 1966, TRW Systems, Redondo Beach, Calif. 7 Rawlin, V. K. and Pawlik, E. V., "A Mercury PlasmaBridge Neutralizer," Journal of Spacecraft and Rockets, Vol. 5, No. 7, 1968, pp. 814-820. 8 Masek, T. D. and Pawlik, E. V., "Thrust System Technology for Solar Electric Propulsion," AIAA Paper 68-541, Cleveland, Ohio, 1968. 9 Trump, G. E., "Flow Meter and Prototype Mercury Feed System Development," EOS-6969-Summary, NASA CR-54713, 1967, Electro-Optical System Inc., Pasadena Calif. 10 Rawlin, V. K. and Kerslake, W. R., "Durability of the SERT II Hollow Cathode and Future Applications at Higher Mission Levels," AIAA Paper 69-304, Williamsburg, Va., 1969; also "SERT II: Durability of the Hollow Cathode and Future Applications of Hollow Cathodes," Journal of Spacecraft and Rockets, Vol. 7, No. 1, Jan. 1970, pp. 14-20. 11 Kemp, R. F. and Hall, D. F., "Ion Beam Diagnostics and Neutralization," TRW-06188-6011-ROOO, NASA CR-72343, 1967, TRW Systems, Redondo Beach, Calif. 12 Bechtel, R. T., "Performance and Control of a 30-Centimeter Diameter Low Impulse Kaufman Thruster," AIAA Paper 69-238, Williamsburg, Va., 1969; also Journal of Spacecraft and Rockets, Vol. 7, No. 1, Jan. 1970, pp. 21-25. 13 Byers, D. C., "An Experimental Investigation of a HighVoltage Electron-Bombardment Ion Thruster," Journal of the Electrochemical Society, Vol. 116, No. 1, Jan. 1969, pp. 9-17. 14 Reader, P. D., "Investigation of a 10-Centimeter-Diameter Electron-Bombardment Ion Rocket," TN D-1163, 1962, NASA. 15 Ward, J. W. and King, H. J., "Mercury Hollow Cathode Plasma Neutralizers," Journal of Spacecraft and Rockets, Vol. 5, No. 10, Oct. 1968, pp. 1161-1164.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::a652c1b9737be4b3f8ad9c7190af435e https://doi.org/10.2514/3.29856 Zobrazit plný text záznamu