| Display title | Engineering:SNCASE SE.212 Durandal |
| Default sort key | Sncase Se-212 Durandal |
| Page length (in bytes) | 13,076 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 202000 |
| 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>Steve Marsio |
| Date of page creation | 21:33, 4 February 2024 |
| Latest editor | imported>Steve Marsio |
| Date of latest edit | 21:33, 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 SNCASE SE.212 Durandal was a French jet and rocket mixed-power experimental fighter aircraft of the mid-1950s.
It was designed by the French aircraft manufacturer SNCASE during the early 1950s, who were keen to exploit the potential advantages of a mixed-power propulsion system. In parallel, as part... |
