Difference between revisions of "S3 KS-25x4 "Mammoth" Liquid Fuel Engine"
From Kerbal Space Program Wiki
(Created page with "{{Future article|v=0.23.5}} {{:S3 KS-25x4 Engine Cluster/Box}} The '''S3 KS-25x4 Engine Cluster''' is a liquid fuel engine with four nozzles. This is the engine with the ...") |
Sciencegey (talk | contribs) m (Post ARM cleanup) |
||
| Line 8: | Line 8: | ||
== Changes == | == Changes == | ||
| − | ;[[0.23.5]] | + | ;[[0.23.5]] |
*Initial release | *Initial release | ||
{{Parts}} | {{Parts}} | ||
[[Category:Liquid fuel engine]] | [[Category:Liquid fuel engine]] | ||
Revision as of 19:49, 2 April 2014
| S3 KS-25x4 "Mammoth" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Kerbodyne | ||
| Radial size | Extra large | |
| Cost | (total) | 39 000.00 
|
| Mass | (total) | 15.000 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 20 m/s | |
| Research |  Very Heavy Rocketry
| |
| Unlock cost | 115 000
| |
| Since version | 0.23.5 | |
| Part configuration | part.cfg | |
| Maximum thrust | (1 atm) | 3 746.03 kN |
| (vacuum) | 4 000.00 kN | |
| Isp | (1 atm) | 295 s |
| (vacuum) | 315 s | |
| Fuel consumption | 258.98  /s
| |
| Thrust vectoring | 2 ° | |
| Electricity generated | 12.0 ⚡/s | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | Yes | |
| In an orbit | Yes | |
| On an escape | Yes | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
The S3 KS-25x4 Engine Cluster is a liquid fuel engine with four nozzles. This is the engine with the highest thrust and, compared to the thrust, high specific impulse. It doesn't allow placing additional stages beneath the engine cluster. This is the liquid fuelled engine second engine after the R.A.P.I.E.R. Engine which uses multiple nozzles.
Manufacturer's description
| “ | Designed for usage as a first stage, this engine uses four of Kerbodyne's KS-25 rocket motors. This is the first in a series of designs that move away from the pattern of simply increasing the engine and nozzle size on a rocket. — Kerbodyne |
” |
Changes
- Initial release
