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

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m (BobBot moved page Toroidal Aerospike Rocket/Box to T-1 Toroidal "Aerospike" Liquid Fuel Engine/Box: Renamed part after update.)
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<noinclude>{{Data template used}}</noinclude>
 
<noinclude>{{Data template used}}</noinclude>
 
{{Infobox/Part
 
{{Infobox/Part
|file=ToroidalAerospikeRocket.png
+
|file=ToroidalAerospikeLiquidFuelEngine.png
 
|type=lfe
 
|type=lfe
|size=s
+
|size=r
 +
|size2=1
 
|manufacturer=C7
 
|manufacturer=C7
 
|costs=3850
 
|costs=3850
|mass=1.5
+
|mass=1.0
 
|drag=0.2
 
|drag=0.2
|temp=3600
+
|temp=2000
 
|tolerance=20
 
|tolerance=20
 
|research=Hypersonic Flight
 
|research=Hypersonic Flight
|unlock cost=42000
+
|unlock cost=24500
 
|since=0.15
 
|since=0.15
 
|filename=liquidEngineAerospike.cfg
 
|filename=liquidEngineAerospike.cfg
 
|part=liquidEngineAerospike
 
|part=liquidEngineAerospike
 +
|parent=Engine
 
|more={{Infobox/Part/reaction engine
 
|more={{Infobox/Part/reaction engine
|thrust=175
+
|thrust=180
|isp-atm=388
+
|isp-atm=290
|isp-vac=390
+
|isp-vac=340
|vectoring=
+
|fuel=lfox
|fuel=lfox
+
}}
 +
{{Infobox/Part/generator
 +
|generate=5.0
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
+
|environments=127
|staging=True
+
|event=y
|event=True
+
|staging=y
 +
}}
 +
{{Infobox/Part/cargo
 +
|volume=1600
 
}}
 
}}
 
}}
 
}}

Latest revision as of 20:23, 9 October 2024

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, Small
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
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
Electricity generated 5.0 ⚡/s
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 1600 l