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

From Kerbal Space Program Wiki
Jump to: navigation, search
m (*update to 1.0;)
m
 
(7 intermediate revisions by 5 users not shown)
Line 1: Line 1:
 
<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=1
 +
|size2=r
 
|manufacturer=C7
 
|manufacturer=C7
 
|costs=3850
 
|costs=3850
|mass=1.5
+
|mass=1.0
 
|drag=0.2
 
|drag=0.2
 
|temp=2000
 
|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
|more={{Infobox/Part/reaction engine
+
|more={{Infobox/Part/title|lfe}}
|thrust=153.788
+
{{Infobox/Part/reaction engine
 +
|fuel=lfox
 
|isp-atm=290
 
|isp-atm=290
|isp-vac=330
+
|isp-vac=340
 +
|thrust=180
 
|vectoring=
 
|vectoring=
|fuel=lfox
 
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
+
|environments=127
 +
|event=True
 
|staging=True
 
|staging=True
|event=True
 
 
}}
 
}}
 
}}
 
}}

Latest revision as of 15:48, 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 Small, Radial mounted
Cost (total) 3 850.00 Funds
Mass (total) 1.00 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
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