Display title | Engineering:XCOR EZ-Rocket |
Default sort key | Xcor Ez-Rocket |
Page length (in bytes) | 8,645 |
Namespace ID | 3034 |
Namespace | Engineering |
Page ID | 1009241 |
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>Wincert |
Date of page creation | 12:03, 4 February 2024 |
Latest editor | imported>Wincert |
Date of latest edit | 12:03, 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. | The XCOR EZ-Rocket was a test platform for the XCOR XR-4A3 rocket propulsion system. The airplane was a modified Rutan Long-EZ, with the propeller replaced by first one, then later a pair of pressure-fed regeneratively cooled liquid-fueled rocket engines and an underslung fuel tank. The engines were... |