Difference between revisions of "T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine/Box"

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m (Add size, Update tests)
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|file=ToroidalAerospikeLiquidFuelEngine.png
 
|file=ToroidalAerospikeLiquidFuelEngine.png
 
|type=lfe
 
|type=lfe
|size=s
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|size=1
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|size=r
 
|manufacturer=C7
 
|manufacturer=C7
 
|costs=3850
 
|costs=3850
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|filename=liquidEngineAerospike.cfg
 
|filename=liquidEngineAerospike.cfg
 
|part=liquidEngineAerospike
 
|part=liquidEngineAerospike
|more={{Infobox/Part/reaction engine
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|more={{Infobox/Part/title|lfe}}
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{{Infobox/Part/reaction engine
 
|fuel=lfox
 
|fuel=lfox
 
|isp-atm=290
 
|isp-atm=290
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}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
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|environments=127
 
|event=True
 
|event=True
 
|staging=True
 
|staging=True
 
}}
 
}}
 
}}
 
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Revision as of 15:08, 18 August 2018

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine
Part image
Liquid fuel engine by
C7 Aerospace Division

Radial size Radial mounted
Cost (total) 3 850.00 Funds
Mass (total) 1.000 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 20 m/s
Research Hypersonic flight.png Hypersonic Flight
Unlock cost 24 500 Funds
Since version 0.15
Part configuration liquidEngineAerospike.cfg
Liquid fuel engine
Maximum thrust (1 atm) 153.53 kN
(vacuum) 180.00 kN
Isp (1 atm) 290 s
(vacuum) 340 s
Fuel consumption 10.80 Units of fuel/s
Thrust vectoring No
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