| Display title | Engineering:Star (rocket stage) |
| Default sort key | Star (rocket stage) |
| Page length (in bytes) | 15,434 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 356621 |
| 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 |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>NBrushPhys |
| Date of page creation | 23:14, 15 March 2024 |
| Latest editor | imported>NBrushPhys |
| Date of latest edit | 23:14, 15 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 Star is a family of United States solid-propellant rocket motors originally developed by Thiokol and used by many space propulsion and launch vehicle stages. They are used almost exclusively as an upper stage, often as an apogee kick motor.
Three Star 37 stages, and one Star 48 stage, were launched... |
