Monday, April 29, 1985
Sunday, April 28, 1985
Tansei 4
1980-015A
Tansei-4 (MS-T4) flew on the first Mu-3S launch. It tested the spin-stabilized attitude control mode for ASTRO-A and the momentum wheel stabilization needed for ASTRO-B and EXOS-C. It also carried an X-ray astronomy experiment.
Tansei-4 is 1.00 dia 0.81 high with a mass of 185 kg, octagonal cylinder plus 4 panels.
The M-3A2 motor is 1.14m dia 2.50m long, with mass 1240 kg full 157 empty. Burn time was 45s, thrust 66.9 kN.
| Tansei-4 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1980 Feb 17 | 0040 | Launch by Mu-3S-1 | KASC |
| T+0:08 SB burnout | |||
| T+0:09 SB sep | |||
| T+1:10 B1 burnout | |||
| T+1:20 B1 sep | |||
| T+1:26 B2 start | |||
| T+2:38 B2 burnout | |||
| T+2:42 Fairing sep (2 parts) | |||
| T+3:11 B2 orbit epoch | |||
| T+4:00 Spinup | |||
| 0047 | T+7:37 B2 sep | ||
| 0047 | T+7:42 B3 start | -5468 x 523 x 38.73 | |
| T+8:09 B2 apogee | |||
| 0048 | T+8:35 B3 burnout | ||
| 0049 | T+9:32 B3 sep | 95.7 517 x 602 x 38.7 | |
| 0049 | T+9:34 B3 yo release | ||
| 0230? | Yo-yo despin, 2 masses released | ||
| 1983 May 12 | Reentered | ||
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