STN EN 16603-20-20
| Označenie: | STN EN 16603-20-20 |
| Platnosť: | Platná |
| Počet strán: | 61 |
| Jazyk: |
EN
|
| Listinná verzia: | 24,40€ |
| Elektronická verzia: |
a) Bez možnosti tlače, prenosu textu a obrázkov:
21,96€ b) Bez možnosti tlače, s prenosom textu a obrázkov: 24,40€ c) S možnosťou tlače, prenosu textu a obrázkov: 31,72€ |
| Slovenský názov: | Kozmická technika. Požiadavky na návrh a rozhranie pre elektrické napájanie |
| Anglický názov: | Space engineering - Electrical design and interface requirements for power supply |
| Dátum vydania: | 01. 02. 2019 |
| Dátum zrušenia: | |
| ICS: | 49.140 |
| Triediaci znak: | 31 0543 |
| Úroveň zapracovania: | idt EN 16603-20-20:2018 |
| Vestník: | 01/19 |
| Zmeny: | |
| Nahradzujúce normy: | |
| Nahradené normy: | |
| Poznámka vo Vestníku: | |
| Predmet normy: | The target applications covered by this standard are all missions traditionally provided with power distribution and protection by LCLs/RLCLs (science, earth observation, navigation) with exclusion of telecom applications which are traditionally provided with power distribution and protection by fuses. The present standard applies to power distribution by LCLs/RLCLs for power systems, and in general for satellites, required to be Single Point Failure Free. The present standard document applies exclusively to the main bus power distribution by LCLs/RLCLs to external satellite loads. Internal power system protections of LCLs/RLCLs are not covered. Paralleling of LCLs to increase power supply line reliability is not covered by the present standard, since this choice does not appreciably change the reliability of the overall function (i.e. LCL plus load). In fact, a typical reliability figure of the LCL (limited to the loss of its switch ON capability) is 20 FIT or less. |
| Náhľad normy: | Náhľad normy (PDF) |