| Display title | Engineering:R-7A Semyorka |
| Default sort key | R-7A Semyorka |
| Page length (in bytes) | 2,672 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 607424 |
| 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>Rtexter1 |
| Date of page creation | 18:05, 5 March 2023 |
| Latest editor | imported>Rtexter1 |
| Date of latest edit | 18:05, 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. | The R-7A Semyorka, GRAU index 8K74, was an early Soviet intercontinental ballistic missile derived from the earlier R-7 Semyorka. It was the only member of the R-7 family of rockets to be deployed as an operational missile. The R-7A first flew on 23 December 1959, entered service on 31 December of the... |
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