| Display title | Engineering:Northrop X-4 Bantam |
| Default sort key | Northrop X-4 Bantam |
| Page length (in bytes) | 12,971 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 920460 |
| 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>Rjetedi |
| Date of page creation | 14:44, 25 June 2023 |
| Latest editor | imported>Rjetedi |
| Date of latest edit | 14:44, 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 Northrop X-4 Bantam was a prototype small twinjet aircraft manufactured by Northrop Corporation in 1948. It had no horizontal tail surfaces, depending instead on combined elevator and aileron control surfaces (called elevons) for control in pitch and roll attitudes, almost exactly in the manner of... |
