| Поле | Инд. | ПП | Название | Значение |
|---|---|---|---|---|
| Тип записи | a | |||
| Библиографический уровень | a | |||
| 001 | Контрольный номер | 17f79779cd3941e18c2e24242b9b24e2 | ||
| 005 | Дата корректировки | 20260224152757.9 | ||
| 040 | a | Служба первич. каталог. | 10013504 | |
| 041 | 0_ | a | Код языка текста | eng |
| 100 | 1_ | a | Автор | Hamley J. |
| 245 | 10 | a | Заглавие | Power electronics development for the SPT-100 thruster |
| 504 | a | Библиография | Библиогр.: с.409 (13 назв.) | |
| 520 | 0_ | a | Аннотация | Russian electric propulsion technologies has recently become available in the world market. Of significant interest in the Stationary Plasma Thruster, (SPT) which has a significant flight heritage in the former Soviet space programm.The SPT has performance levels of up to 1600 seconds of specific impulse at a thrust efficciency of 0,50.Studies have shown that this level of performance is well suited for stationkeeping applications, and the SPT-100, whith a 1,35 kW input power level is presently being evaluated for use on Western commercial satellites. Under a program sponsored by the Innovative Science and Technology Division of the Ballistic Missile Defence Organization, a team of U.S. electric propulsion specialists observed the operation of the SPT-100 in Russia. |
| 653 | 0_ | a | Ключевые слова | ELECTRIC PROPULSION TECHNOLOGY; RUSSIA;CATHODE HEATER; PULSE IGNITION; LOAD TESTING; THRUSTER INTEGRATION TESTS; STATIONARY PLASMA THRUSTERS |
| 700 | 12 | a | Другие авторы | Hill G. |
| 700 | 12 | a | Другие авторы | Sankovic J. |
| 773 | 18 | w | Контрольный № источника | 22e503a4ead64b87a6d596aa3fcc96e7 |
| a | Заголовок основной записи | International electric propulsion conference | ||
| t | Название источника | Proceedings of the 23rd International electric propulsion conference. - Papers IEPC-93-001 THROUGH IPEC 93-087 | ||
| d | Место и дата издания | [1993] | ||
| g | Прочая информация | Vol. 1. - С.405-415 | ||
| 901 | t | Тип документа | c |