| Display title | Engineering:Liquid apogee engine |
| Default sort key | Liquid apogee engine |
| Page length (in bytes) | 16,145 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 759861 |
| 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 | Error creating thumbnail: Unable to save thumbnail to destination |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Jslovo |
| Date of page creation | 22:57, 9 October 2021 |
| Latest editor | imported>Jslovo |
| Date of latest edit | 22:57, 9 October 2021 |
| 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. | A liquid apogee engine (LAE), or apogee engine, refers to a type of chemical rocket engine typically used as the main engine in a spacecraft.
The name apogee engine derives from the type of manoeuvre for which the engine is typically used, i.e. an in-space delta-v change made at the apogee of an elliptical... |
