| Поле | Инд. | ПП | Название | Значение |
|---|---|---|---|---|
| Тип записи | a | |||
| Библиографический уровень | a | |||
| 001 | Контрольный номер | 05ff3e9a13d84b4194be8db3fa59938f | ||
| 005 | Дата корректировки | 20260317123349.6 | ||
| 040 | a | Служба первич. каталог. | 10013504 | |
| 041 | 0_ | a | Код языка текста | eng |
| 100 | 1_ | a | Автор | Miller T. |
| 245 | 10 | a | Заглавие | Mission factors affecting cost optimization of solar electric orbital transfer vehicle |
| 500 | a | Примечание | Analyses and results presented herein were made possible with funding from the U.S.Air Force under contract F04701-90-C-0091. | |
| 504 | a | Библиография | Bibliogr.:p.1828 (12 i.) | |
| 520 | 0_ | a | Аннотация | Several mission and system pasrameters affect cost and design optimizaion of a Solar Electric Orbital Transfer Vehicle (SEOTV). Total launch services costs, specific launch costs, beginning-of-life power, specific impulse, and propellant mass are the parameters used to aid in the cost-optimal design of the SEOTV. |
| 653 | 0_ | a | Ключевые слова | LAUNCH VEHICLE DESIGN; LAUNCH COST; SPECIFIC IMPULSE; PROPELLANT MASS |
| 700 | 12 | a | Другие авторы | Seaworth G. |
| 773 | 18 | w | Контрольный № источника | 9b9c164353e84b8687052e08bee508fa |
| a | Заголовок основной записи | International electric propulsion conference | ||
| t | Название источника | Proceedings of the 23rd International electric propulsion conference. - Papers IEPC-93-177 THROUGH IPEC 93-251 | ||
| d | Место и дата издания | [1993] | ||
| g | Прочая информация | Vol. 3. - P. 1825-1828 | ||
| 901 | t | Тип документа | c |