RD-191 topic
Also known as
- Add other possible names for this topic
| Status |
| Used in rocket stages |
| Government designation |
| Manufactured by |
| Designed by |
| Design period |
|
start
|
end
|
|---|---|
|
|
| Use period |
| Diameter |
- 1.45m
| Height |
- 4.0m
| Thrust (vacuum) |
- 2,087,400.0N
| Thrust (sea level) |
- 1,920,800.0N
| Isp (vacuum) |
- 337.0s
| Isp (sea level) |
- 310.7s
| Dry mass |
| Throttle ratio |
| Wet mass |
| Engine cycle |
| Fuel |
| Oxidizer |
| Oxidizer/fuel ratio |
| Expansion ratio |
| Chamber pressure |
- 258.0bar
| Number of chambers |
- 1
With the exception of Wikipedia summaries and some images the
content on this page is typically distributed under
the Creative Commons
Attribution license or Public Domain.
| Gallery | add |
There are no images for this topic yet.
Edit Weblinks
Recent Discussions about RD-191
There are no conversations on this topic. Would you like to start one?
Start the Discussion »