| Display title | Engineering:Crew Dragon In-Flight Abort Test |
| Default sort key | Crew Dragon In-Flight Abort Test |
| Page length (in bytes) | 18,294 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 263449 |
| 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>Jport |
| Date of page creation | 15:09, 4 February 2024 |
| Latest editor | imported>Jport |
| Date of latest edit | 15:09, 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. | SpaceX Crew Dragon In-Flight Abort Test (also known as Crew Dragon Launch Escape Demonstration) was a successful test of the SpaceX Dragon 2 abort system, conducted on 19 January 2020. It was the final assessment for the Crew Dragon capsule and Falcon 9 launch system before they would be certified to... |
