Difference between revisions of "LV-1 "Ant" Liquid Fuel Engine/Box"

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m (*update to 0.25;)
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|size=t
 
|size=t
 
|manufacturer=JKJSP
 
|manufacturer=JKJSP
|costs=350
+
|costs=110
|mass=0.03
+
|mass=0.02
 
|drag=0.2
 
|drag=0.2
|temp=3600
+
|temp=2000
 
|tolerance=7
 
|tolerance=7
|research=Precision Engineering
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|research=Propulsion Systems
 
|unlock cost=4000
 
|unlock cost=4000
 
|since=0.18
 
|since=0.18
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|part=liquidEngineLV-1
 
|part=liquidEngineLV-1
 
|more={{Infobox/Part/reaction engine
 
|more={{Infobox/Part/reaction engine
|thrust=4
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|thrust=0.5
|isp-atm=220
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|isp-atm=85
|isp-vac=290
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|isp-vac=315
 
|vectoring=
 
|vectoring=
 
|fuel=lfox
 
|fuel=lfox

Revision as of 08:22, 28 April 2015

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
LV-1 "Ant" Liquid Fuel Engine
Part image
Liquid fuel engine by
Jebediah Kerman's Junkyard and Spacecraft Parts Co
Radial size Tiny
Cost (total) 110.00 Funds
Mass (total) 0.02 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Propulsion systems.png Propulsion Systems
Unlock cost 4 000 Funds
Since version 0.18
Part configuration liquidEngineLV-1
Maximum thrust (1 atm) 0.13 kN
(vacuum) 0.50 kN
Isp (1 atm) 85 s
(vacuum) 315 s
Fuel consumption 0.03 Units of fuel/s


Thrust vectoring × No
Testing Environments
On the surface × No
In the ocean × No
On the launchpad × No
In the atmosphere ✓ Yes
Sub orbital × No
In an orbit × No
On an escape × No
Docked × No
Test by staging × No
Manually testable ✓ Yes