1990-001B
JCSAT 2 was the second HS-393 spinner and had a mass of 1260 kg on orbit. It was launched aboard a Commercial Titan 3, with an added Orbus 21S perigee kick motor placing it into geostationary transfer orbit.
| JCSAT 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Jan 1 | 0007 | Launch by Commercial Titan 3 | CC LC40 |
| 0008:49 | T+1:49 Stage 1 ignition | ||
| 0008:57 | T+1:57 SRM sep | ||
| 0011:27 | T+4:27 Stage 2 ignition, St 1 sep | ||
| 0011:38 | T+4:38 Fairing sep | ||
| 0015:06 | T+8:06 Stage 2 cutoff | ||
| 0015 | Earth orbit insertion | 165 x 612 x 28.6 | |
| 0118:52 | T+1:11:52 Skynet 4A sep from Titan | ||
| 0220:30 | T+2:13:30? Extension module separated | ||
| 0251:46 | T+2:44:46 JCSAT 2 sep from Titan | ||
| 0337? | Orbus 7S burn | ||
| 0339? | Burnout | ||
| 0345? | Orbus sep | 300 x 19294 x 26.8 | |
| Perigee burn | |||
| Apogee burn | |||
| 1990 Jan 5 | 1436.33 35668 x 35913 x 0.4 GEO 153.9E | ||
| 1990 Jan 7 | 1436.28 35671 x 35909 x 0.3 GEO 153.8E | ||
| 1990 Feb 15 | 1436.12 35775 x 35798 x 0.1 GEO 154.0E | ||
| 1993 Mar 29 | 1436.12 35778 x 35795 x 0.0 GEO 154.0E | ||
| 1996 May 26 | 1436.10 35780 x 35792 x 0.1 GEO 154.0E | ||
| 2000 Jul 4 | 1436.12 35773 x 35800 x 0.1 GEO 154.0E | ||
No comments:
Post a Comment