1976-009A
Medium res photo recon satellite. PDM telemetry, extended duration
| Kosmos-799 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1976 Jan 29 | 0830 | Launch by Soyuz-U | Baikonur |
| 0834 | Blok-I burn | ||
| 0838 | Blok-I sep | ||
| 1976 Jan 29 | 89.62 201 x 309 x 71.4 | ||
| 1976 Feb 9 | 89.52 202 x 299 x 71.4 | ||
| 1976 Feb 10 | |||
| 0530? | Deorbit | ||
| 0540? | PO sep | ||
| 0546? | Entry | ||
| 0602? | Landed | ||
1996-S07
The HYFLEX lifting body was launched on the first test flight of the J-1 rocket. The J-1 performed perfectly and Hyflex reentered the atmosphere, proving performance of the heat shield tiles and control systems. However, the vehicle's flotation device separated after splashdown and Hyflex sank before it could be recovered. 12 of the 14 experiments returned their data via telemetry successfully, but the post-flight condition of the thermal protection system could not be inspected.
Splashdown was at 143.5E 28.5N.
Mass was 1054 kg, size was 4.4 l 1.4m dia.
| Hyflex | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1996 Feb 11 | 2300 | Launch by J-1 (1F) | TSNC O |
| T+1:35 St 1 burnout | |||
| T+2:15 H-1 SRB sep 80 km | -6365 x 95 ? | ||
| T+2:17 M23 burn | |||
| 2303 | T+3:27 M23 burnout | ||
| T+3:36 Fairing sep | |||
| 2304 | Apogee 107 km 3.9km/s | ||
| 2304 | T+3:58 M23 sep 136E 30.5N | -5450 x 107 x 30.6 | |
| Reentry | |||
| 62 km 4 km/s | |||
| Parachute deploy | |||
| 2311? | Splashdown near Ogasawara I | ||
1973-010A
Tselina-OM satellite Kosmos-549 was launched in Feb 1973, keeping up a high launch rate.
| Kosmos-549 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1973 Feb 28 | 0433? | Launch by 11K65M | PL |
| 0435? | Stage 2 burn | ||
| 0441? | Stage 2 coast | ||
| 0506? | Stage 2 burn 2 | ||
| 0506? | Stage 2 sep | ||
| 1973 Mar 1 | 0230 | 95.23 513 x 545 x 74.0 | |
| 1980 Jun 29 | Reentered | ||
