Friday, March 2, 1990
Orizuru
1990-013B
The H-I LE-5 second stage from the Momo-1b flight carried a supplementary technology experiment called DEBUT, the Deployable Boom and Umbrella Test. It was named Orizuru (an origami crane) after launch.
DEBUT was built by NAL. The satellite was a 0.44m 26-sided polyhedron similar to the JAS/Fuji satellites, with a 0.2m box containing the boom system on top. The umbrella deployed at the end of the boom was a test for aerodyamic braking; it was 0.90m dia when open. Mass of the umbrella was 4 kg. The 5 kg boom is 1.20m long deployed; overall deployed height 1.94m. Total mass 50.3kg. The spacecraft operated 10 days.
The boom was deployed and retracted 34 times and the ADB was opened and closed 52 times.
| Orizuru | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Feb 7 | 0133 | Launch by H-I | TNSC |
| SECO-1 | |||
| SES-2 | |||
| MOS-1b sep | |||
| SECO-2 | |||
| DEBUT sep | |||
| 1990 Feb 17 | End of transmissions | ||
Payload:
- Boom mechanism
- ADB Deployable aerodynamic umbrella mechanism
Kosmos 1515
1983-122A
| Kosmos-1515 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1983 Dec 15 | 1225 | Launch by 11K68 | Plesetsk |
| T+2:00 St 1 sep | |||
| T+3:33? GO sep | |||
| T+4:38? St 2 sep | |||
| T+5:20? S5M burn 1 | |||
| 1231 | T+6:48 S5M MECO1 km | 60? x 650 x 82.5 | |
| T+40:58? S5M burn 2 | |||
| T+41:08? S5M MECO2 | |||
| 1306? | T+41:38? S5M sep | ||
| 1983 Dec 18 | 97.8 638x665x82.5 | ||
Wednesday, February 28, 1990
Kosmos 1425
1982-119A
Two-tone telemetry; Medium res satellite
| Kosmos-1425 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1982 Dec 23 | 0910 | Launch by Soyuz-U | Baikonur |
| 0914 | Blok-I burn | ||
| 0918 | Blok-I sep | ||
| 1982 Dec 23 | 90.32 230x351x70.0 | ||
| 1982 Dec 28 | 92.21 348x418x70.0 from 90.32 230x351 | ||
| 1983 Jan 5 | 92.20 349x416x70.0 | ||
| 1983 Jan 6 | |||
| 0555? | Deorbit | ||
| 0605? | PO sep | ||
| 0623? | Entry | ||
| 0635? | Landed | ||
Tuesday, February 27, 1990
Kosmos 1982
1988-105A
Two-tone telemetry; Medium res satellite
| Kosmos-1982 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Nov 30 | 0900:00 | Launch by Soyuz | KB |
| 0904 | Blok-I burn | ||
| 0908 | Blok-I MECO | ||
| 1988 Nov 30 | 90.38 207x380x70.0 | ||
| 1988 Nov 30.9 | 90.30 205x373x70.0 | ||
| 1988 Dec 1.1 | 92.17 356x406x70.0 | ||
| 1988 Dec 1 | 92.16 348x414x70.0 | ||
| 1988 Dec 5 | 92.16 348x414x70.0 | ||
| 1988 Dec 13 | 92.17 348x413x70.0 | ||
| 1988 Dec 14 | |||
| 0550? | Deorbit | ||
| 0600? | PO sep | ||
| 0618? | Entry | -78 x 395 | |
| 0630? | Landed | ||
Monday, February 26, 1990
Sunday, February 25, 1990
Kosmos 182
1967-098A
Zenit-4 No. 36 was launched in Oct 1967 from Baikonur on a standard 8 day, 65.0 degree mission.
| Kosmos-182 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1967 Oct 16 | 0800 | Launch by 11A57 | KB |
| 0804 | Blok-I burn | ||
| 0809 | Blok-I sep | 89.9 210 x 330 x 65.0 (RAE) | |
| 1967 Oct 17 | 89.91 203 x 336 x 65.0 | ||
| 1967 Oct 22 | 89.83 202 x 329 x 65.0 | ||
| 1967 Oct 24 | 0607 | Deorbit | |
| 0627? | Landed after 7.93d | ||