| Display title | Engineering:Falcon 9 Block 5 |
| Default sort key | Falcon 9 Block 5 |
| Page length (in bytes) | 25,350 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 188545 |
| 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>MainAI |
| Date of page creation | 16:22, 4 February 2024 |
| Latest editor | imported>MainAI |
| Date of latest edit | 16:22, 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. | Falcon 9 Block 5 is a partially reusable two-stage-to-orbit medium-lift launch vehicle designed and manufactured in the United States by SpaceX. It is the fifth version of Falcon 9 Full Thrust, powered by SpaceX Merlin engines burning rocket-grade kerosene (RP-1) and liquid oxygen (LOX).
The main changes... |
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