Difference between revisions of "48-7S "Spark" Liquid Fuel Engine/Box"
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file= | + | |file=48-7S_Shroud.png |
|type=lfe | |type=lfe | ||
| − | |size= | + | |size=0 |
|manufacturer=RMC | |manufacturer=RMC | ||
| − | |costs= | + | |costs=240 |
| − | |mass=0. | + | |mass=0.13 |
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
| − | |research= | + | |research=Propulsion Systems |
|unlock cost=2800 | |unlock cost=2800 | ||
|since=0.21 | |since=0.21 | ||
| − | |filename=liquidEngine48- | + | |filename=liquidEngine48-7S_v2.cfg |
| − | |part=liquidEngine48- | + | |part=liquidEngine48-7S_v2 |
| + | |parent=Engine | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
| − | |thrust= | + | |thrust=20 |
| − | |isp-atm= | + | |isp-atm=265 |
| − | |isp-vac= | + | |isp-vac=320 |
| − | |vectoring= | + | |vectoring=3 |
| − | |fuel=lfox | + | |fuel=lfox |
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments= | + | |environments=127 |
| − | |staging= | + | |event=y |
| − | | | + | |staging=y |
| + | }} | ||
| + | {{Infobox/Part/cargo | ||
| + | |volume=140 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:17, 9 October 2024
| 48-7S "Spark" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Rockomax Conglomerate | ||
| Radial size | Tiny | |
| Cost | (total) | 240.00 
|
| Mass | (total) | 0.130 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Propulsion Systems
| |
| Unlock cost | 2 800
| |
| Since version | 0.21 | |
| Part configuration | liquidEngine48-7S_v2.cfg | |
| Maximum thrust | (1 atm) | 16.56 kN |
| (vacuum) | 20.00 kN | |
| Isp | (1 atm) | 265 s |
| (vacuum) | 320 s | |
| Fuel consumption | 1.27  /s
| |
| Thrust vectoring | 3 ° | |
| 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 | 140 l | |
