| Display title | Engineering:RatSat |
| Default sort key | RatSat |
| Page length (in bytes) | 16,385 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 2219194 |
| 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>MedAI |
| Date of page creation | 13:58, 4 February 2024 |
| Latest editor | imported>MedAI |
| Date of latest edit | 13:58, 4 February 2024 |
| Total number of edits | 2 |
| 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. | RatSat or DemoSat was an aluminum mass simulator on the fourth flight of the Falcon 1 rocket, launched on 28 September 2008. Ratsat remained bolted to the second stage of the carrier rocket after reaching low Earth orbit. It is an aluminium alloy chamber in hexagonal prism shape with 1.5 m (5 ... |
