| Display title | Engineering:Tupolev Tu-244 |
| Default sort key | Tupolev Tu-244 |
| Page length (in bytes) | 4,688 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 620462 |
| 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>AnLinks |
| Date of page creation | 11:40, 25 June 2023 |
| Latest editor | imported>AnLinks |
| Date of latest edit | 11:40, 25 June 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 Tupolev Tu-244 was a proposed supersonic transport (SST) aircraft, developed from the Tu-144. It implemented novel features such as cryogenic fuel to enable flight distances of up to 10,000 km (6,200 mi) and would have carried up to 300 passengers. The project was cancelled in 1993. |
