1966-033A
Zenit-2 No. 35 was launched in Apr 1966 and flew a successful week-long mission.
| Kosmos-115 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Apr 20 | 1040 | Launch by Vostok 8A92 | KB |
| 1045? | Blok-E burn | ||
| 1050? | Blok-E sep | ||
| 89.3 190 x 294 x 65 (TASS) | |||
| 1200 | 89.4 201 x 294 x 65.0 (RAE) | ||
| 1966 Apr 22 | 1904 | 89.25 187 x 286 x 65.0 | |
| 1966 Apr 26 | 0620 | 89.16 182 x 282 x 65.0 | |
| 1966 Apr 28 | 0907? | Landed after 7.93d | |
2003-005B
The XSS-10 inspector microsatellite is built by AFRL. It tests a new propulsion system , hydrazine Guidance, navigation & control (GNC) Miniaturized communications system Primary lithium polymer batteries Integrated camera and star sensor.
Mass is 28 kg. Size is 1.0 long 0.45m dia.
| XSS-10 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2003 Jan 29 | 1806:00 | Launch by Delta 7925-9.5 | CC LC17 |
| T+1:03 SRM 1-6 out | |||
| T+1:06 SRM 7-9 on | |||
| T+1:07 SRM 1-6 sep | |||
| T+2:12 SRM 7-9 out | |||
| T+4:24 MECO | |||
| T+4:32 St 1 sep | |||
| T+4:38 SES-1 | |||
| T+4:59 Fairing sep | |||
| 1816:53 | T+10:53 SECO-1 | 172 x 198 x 36.9 | |
| 1908:39 | T+1:02:39 SES-2 | ||
| 1909:15 | T+1:03:15 SECO-2 | 187 x 1157 x 37.2 | |
| 1910:08 | T+1:04:08 Stage 2 sep | ||
| SES-3 | |||
| SECO-3 | |||
| SES-4 | |||
| SECO-4? | 703 x 806 x 39.6 | ||
| 2003 Jan 30 | 10035 | XSS-10 sep | |
| Drift 200m away | |||
| 1110 | Inspection approach 1, 100m | ||
| 1120 | Inspection approach 1b, 35m | ||
| 1126 | Drift few 100 m away | ||
| 1245 | Inspection approach 2, 35 and 100m? | ||
| 1325 | Inspection approach 3, 35 and 100m? | ||
| 1340 | Sleep mode | ||
| 1620 | Reactivated | ||
| 1805 | depletion burn | 516 x 804 x 39.8 | |
