Difference between revisions of "LFB KR-1x2 "Twin-Boar" Liquid Fuel Engine/Box"
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m (BobBot moved page LFB KR-1x2/Box to LFB KR-1x2 "Twin-Boar" Liquid Fuel Engine/Box: Renamed part after update.) |
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{{Infobox/Part | {{Infobox/Part | ||
|file=LFB_KR-1x2.png | |file=LFB_KR-1x2.png | ||
| − | | | + | |type=lfe |
| − | |size= | + | |size=2 |
| + | |size2=r | ||
|manufacturer=KD | |manufacturer=KD | ||
| − | |costs= | + | |costs=17000 |
| − | |mass=10. | + | |mass=10.5 |
| − | |lf=2880 | + | |lf=2880 |
| + | |ox=3520 | ||
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=20 | |tolerance=20 | ||
|research=Heavier Rocketry | |research=Heavier Rocketry | ||
| Line 15: | Line 17: | ||
|since=0.23.5 | |since=0.23.5 | ||
|filename=part.cfg | |filename=part.cfg | ||
| − | |part= | + | |part=Size2LFB_v2 |
| − | | | + | |parent=Engine |
| − | |more={{Infobox/Part/ | + | |more={{Infobox/Part/reaction engine |
| − | | | + | |thrust=2000 |
| − | | | + | |isp-atm=280 |
| − | | | + | |isp-vac=300 |
| + | |vectoring=1.5 | ||
| + | |fuel=lfox | ||
}} | }} | ||
| − | {{Infobox/Part/ | + | {{Infobox/Part/test subject |
| − | + | |environments=127 | |
| − | + | |event=y | |
| − | + | |staging=y | |
| − | | | ||
| − | | | ||
| − | | | ||
}} | }} | ||
| − | |||
{{Infobox/Part/tank | {{Infobox/Part/tank | ||
| − | |lf=2880 | + | |lf=2880 |
| + | |ox=3520 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:18, 9 October 2024
| LFB KR-1x2 "Twin-Boar" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Kerbodyne | ||
| Radial size | Large, Radial mounted | |
| Cost | (total) | 17 000.00 
|
| (dry) | 14 062.40
| |
| Mass | (total) | 42.500 t |
| (dry) | 10.500 t | |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 20 m/s | |
| Research |  Heavier Rocketry
| |
| Unlock cost | 65 000
| |
| Since version | 0.23.5 | |
| Part configuration | part.cfg | |
| Maximum thrust | (1 atm) | 1 866.67 kN |
| (vacuum) | 2 000.00 kN | |
| Isp | (1 atm) | 280 s |
| (vacuum) | 300 s | |
| Fuel consumption | 135.96  /s
| |
| Thrust vectoring | 1.5 ° | |
| 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 | |
| Liquid fuel | 2 880
| |
| Oxidizer | 3 520
| |
