File:SABRE Rocket nozzle mode.png
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Summary
| Description |
English: the central rocket combustion chamber is in use with the bell moved forwards to create a larger, more efficient nozzle for high altitude flight. |
| Date | |
| Source | https://patents.google.com/patent/US20150101337A1/en?assignee=Reaction+Engines+Limited |
| Author | Reaction Engines Limited |
Licensing
This file is licensed under the Creative Commons Attribution-Share Alike 4.0 International license.
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- to share â to copy, distribute and transmit the work
- to remix â to adapt the work
- Under the following conditions:
- attribution â You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
- share alike â If you remix, transform, or build upon the material, you must distribute your contributions under the same or compatible license as the original.
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 23:07, 27 January 2020 | | 1,642 Ã 2,248 (35 KB) | Harryloud1 | User created page with UploadWizard |
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