| Display title | Engineering:Solid rocket booster |
| Default sort key | Solid Rocket Booster |
| Page length (in bytes) | 8,403 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 728418 |
| 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>Steve2012 |
| Date of page creation | 12:32, 4 February 2024 |
| Latest editor | imported>Steve2012 |
| Date of latest edit | 12:32, 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. | A solid rocket booster (SRB) is a large solid propellant motor used to provide thrust in spacecraft launches from initial launch through the first ascent. Many launch vehicles, including the Atlas V, SLS and Space Shuttle, have used SRBs to give launch vehicles much of the thrust required to place the... |
