Difference between revisions of "24-77 "Twitch" Liquid Fuel Engine/Box"
From Kerbal Space Program Wiki
m (BobBot moved page Rockomax 24-77/Box to 24-77 "Twitch" Liquid Fuel Engine/Box: Renamed part after update.) |
m (Update part) |
||
| (9 intermediate revisions by 4 users not shown) | |||
| Line 1: | Line 1: | ||
<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file= | + | |file=24-77 Orange.png |
|type=lfe | |type=lfe | ||
| + | |size=r | ||
|manufacturer=RMC | |manufacturer=RMC | ||
| − | |costs= | + | |costs=230 |
| − | |mass=0. | + | |mass=0.08 |
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
| − | |research=Precision | + | |research=Precision Propulsion |
| − | |unlock cost= | + | |unlock cost=920 |
|since=0.18 | |since=0.18 | ||
| − | |filename=liquidEngine24- | + | |filename=liquidEngine24-77_v2.cfg |
| − | |part=liquidEngine24- | + | |part=liquidEngine24-77_v2 |
| + | |parent=Engine | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
| − | |thrust= | + | |thrust=16 |
| − | |isp-atm= | + | |isp-atm=275 |
| − | |isp-vac= | + | |isp-vac=290 |
| − | |vectoring= | + | |vectoring=8 |
| − | |fuel=lfox | + | |fuel=lfox |
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments= | + | |environments=127 |
| − | |staging= | + | |event=y |
| − | | | + | |staging=y |
| + | }} | ||
| + | {{Infobox/Part/cargo | ||
| + | |volume=65 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:17, 9 October 2024
| 24-77 "Twitch" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Rockomax Conglomerate | ||
| Radial size | Radial mounted | |
| Cost | (total) | 230.00 
|
| Mass | (total) | 0.080 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Precision Propulsion
| |
| Unlock cost | 920
| |
| Since version | 0.18 | |
| Part configuration | liquidEngine24-77_v2.cfg | |
| Maximum thrust | (1 atm) | 15.17 kN |
| (vacuum) | 16.00 kN | |
| Isp | (1 atm) | 275 s |
| (vacuum) | 290 s | |
| Fuel consumption | 1.13  /s
| |
| Thrust vectoring | 8 ° | |
| 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 | 65 l | |
