Difference between revisions of "RE-L10 "Poodle" Liquid Fuel Engine/Box"
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file= | + | |file=RE-L10.png |
|type=lfe | |type=lfe | ||
| − | |size= | + | |size=2 |
|manufacturer=RMC | |manufacturer=RMC | ||
| − | |costs= | + | |costs=1300 |
| − | |mass= | + | |mass=1.75 |
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
|research=Heavy Rocketry | |research=Heavy Rocketry | ||
|unlock cost=4200 | |unlock cost=4200 | ||
|since=0.16 | |since=0.16 | ||
| − | |filename= | + | |filename=liquidEnginePoodle_v2.cfg |
| − | |part= | + | |part=liquidEnginePoodle_v2 |
| + | |parent=Engine | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
| − | |thrust= | + | |thrust=250 |
| − | |isp-atm= | + | |isp-atm=90 |
| − | |isp-vac= | + | |isp-vac=350 |
| − | |vectoring= | + | |vectoring=5 |
| − | |fuel=lfox | + | |fuel=lfox |
| + | }} | ||
| + | {{Infobox/Part/generator | ||
| + | |generate=8.0 | ||
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments= | + | |environments=127 |
| − | |staging= | + | |event=y |
| − | | | + | |staging=y |
| + | }} | ||
| + | {{Infobox/Part/cargo | ||
| + | |volume=-1 | ||
| + | |stack=1 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:22, 9 October 2024
| RE-L10 "Poodle" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Rockomax Conglomerate | ||
| Radial size | Large | |
| Cost | (total) | 1 300.00 
|
| Mass | (total) | 1.750 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Heavy Rocketry
| |
| Unlock cost | 4 200
| |
| Since version | 0.16 | |
| Part configuration | liquidEnginePoodle_v2.cfg | |
| Maximum thrust | (1 atm) | 64.29 kN |
| (vacuum) | 250.00 kN | |
| Isp | (1 atm) | 90 s |
| (vacuum) | 350 s | |
| Fuel consumption | 14.57  /s
| |
| Thrust vectoring | 5 ° | |
| Electricity generated | 8.0 ⚡/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 | |
| Packed volume | None | |
