| タイトル | Cosmic Background Explorer (COBE): Emergency support |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920003874 |
| 著者（英） | Stanford, R.; Mattson, R. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1991-10-01 |
| 言語 | eng |
| 内容記述 | The Cosmic Background Explorer (COBE) Mission will measure the diffuse radiation from the universe in the wavelength band 1 micron to 9.6 mm. The band includes the 3 K cosmic background radiation, the known relic of the primeval cosmic explosion. The COBE satellite will be launched from the Western Space and Missile Center (EWSMC) via a Delta launch vehicle into a circular parking orbit of about 300 km. COBE will be placed into a 900-km altitude circular orbit. Coverage will be provided by the Deep Space Network (DSN) for COBE emergencies that would prevent communications via the normal channels of the Tracking and Data Relay Satellite System (TDRSS). Emergency support will be provided by the DSN 26-m subnetwork. Information is given in tabular form for DSN network support, frequency assignments, telemetry, and command. |
| NASA分類 | ASTRONAUTICS (GENERAL) |
| レポートNO | 92N13092 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/129776 |
