Difference between revisions of "LV-909 "Terrier" Liquid Fuel Engine/Box"
From Kerbal Space Program Wiki
m (*update to 1.0;) |
m (Update part) |
||
(4 intermediate revisions by 2 users not shown) | |||
Line 1: | Line 1: | ||
<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=390 | |costs=390 | ||
Line 11: | Line 12: | ||
|research=Advanced Rocketry | |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=85 | + | |isp-atm=85 |
− | |isp-vac=345 | + | |isp-vac=345 |
− | |vectoring=4 | + | |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 |