| Display title | Engineering:Soyuz TMA-3 |
| Default sort key | Soyuz TMA-03 |
| Page length (in bytes) | 6,796 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 562571 |
| Page content language | en - English |
| Page content model | wikitext |
| Indexing by robots | Allowed |
| Number of redirects to this page | 0 |
| Counted as a content page | Yes |
| Page image |  |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Importwiki |
| Date of page creation | 19:08, 5 March 2023 |
| Latest editor | imported>Importwiki |
| Date of latest edit | 19:08, 5 March 2023 |
| Total number of edits | 1 |
| Recent number of edits (within past 90 days) | 0 |
| Recent number of distinct authors | 0 |
Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | Soyuz TMA-3 was a Soyuz (Russian Союз ТМА-3, Union TMA-3) mission to the International Space Station (ISS) launched by a Soyuz FG launch vehicle which was the third flight for the TMA modification of the Soyuz spacecraft, and the 7th Soyuz to fly to the ISS. |
