| Display title | Engineering:Yakovlev Yak-46 |
| Default sort key | Yakovlev Yak-46 |
| Page length (in bytes) | 25,957 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 922392 |
| 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 |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Len Stevenson |
| Date of page creation | 20:51, 4 February 2024 |
| Latest editor | imported>Len Stevenson |
| Date of latest edit | 20:51, 4 February 2024 |
| 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 Yakovlev Yak-46 was a proposed aircraft design based on the Yak-42 with two contra-rotating propellers on the propfan located at the rear. The specification of the Samara turbofans was in the 11,000 kg (24,250 lb) thrust range. Though proposed in the 1990s, production of the Yak-46 never commenced... |
