| Display title | Engineering:AJ10 |
| Default sort key | AJ10 |
| Page length (in bytes) | 9,050 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 40297 |
| 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>JMinHep |
| Date of page creation | 00:00, 16 March 2024 |
| Latest editor | imported>JMinHep |
| Date of latest edit | 00:00, 16 March 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 AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet). It has been used to propel the upper stages of several launch vehicles, including the Delta II and Titan III. Variants were and are used as the service propulsion engine for the Apollo command and service... |
