| Display title | Engineering:Little Joe 1A |
| Default sort key | Little Joe 1a |
| Page length (in bytes) | 3,712 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 187849 |
| 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>WikiEd2 |
| Date of page creation | 15:17, 25 June 2023 |
| Latest editor | imported>WikiEd2 |
| Date of latest edit | 15:17, 25 June 2023 |
| 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. | Little Joe 1A (LJ-1A) was an uncrewed rocket launched as part of NASA's Mercury program on November 4, 1959. This flight, a repeat of the Little Joe 1 (LJ-1) launch, was to test a launch abort under high aerodynamic load conditions. After lift-off, the pressure sensing system was to indicate when the... |
