Представление документа в формате MARC21

Поле Инд. ПП Название Значение
Тип записи a
Библиографический уровень a
001 Контрольный номер 5bfb2c3c69a34f73bfe7206c0c918860
005 Дата корректировки 20260304123350.9
040 a Служба первич. каталог. 10013504
041 0_ a Код языка текста eng
100 1_ a Автор Manzella D.
245 10 a Заглавие Stationary plasma thruster plume emission
260 c Дата издания [1993]
504 a Библиография Библиогр.: с. 921-922 (32 i.)
520 0_ a Аннотация The emission spectrum from a xenon plasma produced by a Stationary Plasma Thruster provided by the Ballistic Missile Defence Organization (BMDO) was measured. Approximately 270 individual Xe I, Xe II and Xe III transitions were identified. A total of 250 mW of radiated optical emission was estimated from measurements taken at the thruster exit plane. There was no evidence of erosion products in the emission signature. Ingestion and ionization of background gas at elevated background pressure was detected.
653 0_ a Ключевые слова STATIONARY PLASMA THRUSTER; PLUME CHARACTERISTICS; PLUME EMISSION;SPT-100
773 18 w Контрольный № источника 4dc810817c434fa388b4e457a4b757a9
a Заголовок основной записи International electric propulsion conference
t Название источника Proceedings of the 23rd International electric propulsion conference. - Papers IEPC-93-088 THROUGH IPEC 93-176
d Место и дата издания [1993]
g Прочая информация Vol. 2. - P.913-923
901 t Тип документа c