Difference between revisions of "LV-909 "Terrier" Liquid Fuel Engine/Box"
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file=LV- | + | |file=LV-909_Shroud.png |
|type=lfe | |type=lfe | ||
| + | |size=1 | ||
|manufacturer=JKJSP | |manufacturer=JKJSP | ||
| − | |costs= | + | |costs=390 |
|mass=0.5 | |mass=0.5 | ||
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
| − | |research= | + | |research=Advanced Rocketry |
|unlock cost=1600 | |unlock cost=1600 | ||
| − | |since=0.14 | + | |since=0.14 |
| − | |filename=liquidEngineLV- | + | |filename=liquidEngineLV-909_v2.cfg |
| − | |part=liquidEngineLV- | + | |part=liquidEngineLV-909_v2 |
| + | |parent=Engine | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
| − | |thrust= | + | |thrust=60 |
| − | |isp-atm= | + | |isp-atm=85 |
| − | |isp-vac= | + | |isp-vac=345 |
| − | |vectoring= | + | |vectoring=4 |
| − | |fuel=lfox | + | |fuel=lfox |
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments= | + | |environments=127 |
| − | |staging= | + | |event=y |
| − | | | + | |staging=y |
| + | }} | ||
| + | {{Infobox/Part/cargo | ||
| + | |volume=1300 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:19, 9 October 2024
| LV-909 "Terrier" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Jebediah Kerman's Junkyard and Spacecraft Parts Co | ||
| Radial size | Small | |
| Cost | (total) | 390.00 
|
| Mass | (total) | 0.500 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Advanced Rocketry
| |
| Unlock cost | 1 600
| |
| Since version | 0.14 | |
| Part configuration | liquidEngineLV-909_v2.cfg | |
| Maximum thrust | (1 atm) | 14.78 kN |
| (vacuum) | 60.00 kN | |
| Isp | (1 atm) | 85 s |
| (vacuum) | 345 s | |
| Fuel consumption | 3.55  /s
| |
| Thrust vectoring | 4 ° | |
| 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 | 1300 l | |
