
Tsiolkovsky-Ryazan 1 and 2 []
The Tsiolkovsky-Ryazan 1 and 2 are small Russian experimental satellites, which are to be deployed from the ISS during a spacewalk. They were developed at the Southwestern State University (SWSU, YuZGU) together with the Ryazan State Radio Engineering University.
| Nation: | Russia |
|---|---|
| Type / Application: | Technology, communication |
| Operator: | Southwestern State University (SWSU, YuZGU), Ryazan State Radio Engineering University |
| Contractors: | Southwestern State University (SWSU, YuZGU), Ryazan State Radio Engineering University |
| Equipment: | |
| Configuration: | 3U Cubesat with handle |
| Propulsion: | None |
| Power: | Solar cells, batteries |
| Lifetime: | 6 months |
| Mass: | 4.8 kg |
| Orbit: | 397 km × 407 km, 51.64° (#1); 398 km × 409 km, 51.64° (#2); 401 km × 407 km, 51.64° (#3); 401 km × 408 km, 51.64° (#4) |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| Tsiolkovsky-Ryazan 1 (RS 9S) | 1998-067TW | 03.06.2022 | Ba LC-31/6 | Soyuz-2-1a | with Progress-MS 20, YuZGU-55 11, YuZGU-55 12, Tsiolkovsky-Ryazan 2 | |
| Tsiolkovsky-Ryazan 2 (RS 12S) | 1998-067TS | 03.06.2022 | Ba LC-31/6 | Soyuz-2-1a | with Progress-MS 20, YuZGU-55 11, YuZGU-55 12, Tsiolkovsky-Ryazan 1 |
