| Поле | Инд. | ПП | Название | Значение |
|---|---|---|---|---|
| Тип записи | a | |||
| Библиографический уровень | a | |||
| 001 | Контрольный номер | 08ae1ac114f94503b7bafb292063ee65 | ||
| 005 | Дата корректировки | 20260302144135.3 | ||
| 040 | a | Служба первич. каталог. | 10013504 | |
| 041 | 0_ | a | Код языка текста | eng |
| 245 | 10 | a | Заглавие | Development of a power electronics unit for the space station plasma contactor |
| 260 | c | Дата издания | [1993] | |
| 520 | 0_ | a | Аннотация | A hollow cathode plasma contactor has been baselined as a charge control device for Space Station (SS) to prevent deleterios interactions of coated structural components with the ambient plasma. NASA Lewis Research Center Work Package 4 initiated the development of a plasma contactor system comprised as a Power Electronics Unit (PEU), an Expellant ManagementUnit (EMU), a command and data interface, and a Plasma Contactor Unit (PCU).A breadboard PEU was designed and fabricated, and contained a cathode heater and discharge power supply, which were required to operate the PCU, a control and auxiliary power converter, an EMU interface, a command and telemetry interface, and a controller. |
| 653 | 0_ | a | Ключевые слова | SPACE STATION; PLASMA CONTACTOR; HOLLOW CATHODE;CATHODE HEATER; ARCJET SYSTEM |
| 700 | 12 | a | Другие авторы | Hamley J. |
| 700 | 12 | a | Другие авторы | Hill G. |
| 700 | 12 | a | Другие авторы | Patterson M.J. |
| 700 | 12 | a | Другие авторы | Saggio J. |
| 700 | 12 | a | Другие авторы | Terdan F. |
| 700 | 12 | a | Другие авторы | Mansell 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. - P.488-499 | ||
| 901 | t | Тип документа | c |