Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"

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<noinclude>{{Data template used}}
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<noinclude>{{Data template used}}</noinclude>
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{{Box|This is not the current design of the infobox. But if you have suggestions how to make it better join the [[Template_talk:Infobox/Part#Rework_the_template.3F|discussion]].}}</noinclude>
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{{Infobox/Part
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{{Infobox/Part/Engine/Liquid
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|file=Rapier Engine_01.png
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|file=Rapier_Engine_01.png
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|type=he
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|manufacturer=C7 Aerospace Division and Rockmax Conglomerate
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|size=1
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|size=s
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|manufacturer=C7
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|costs=5900
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|manufacturer2=RMC
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|mass=1.75
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|costs=6000
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|mass=2.0
 
|drag=0.2
 
|drag=0.2
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|temp=3600
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|temp=2000
 
|tolerance=20
 
|tolerance=20
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|thrust=175
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|research=Aerospace Tech
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|isp-atm=320
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|unlock cost=35000
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|isp-vac=360
 
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|vectoring=3
 
 
|since=0.23
 
|since=0.23
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|filename=rapierEngine.cfg
 
|part=rapierEngine
 
|part=rapierEngine
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|parent=Engine
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|more={{Infobox/Part/jet engine
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|thrust=105
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|isp=3200
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|vectoring=3
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|intake=6
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}}
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{{Infobox/Part/reaction engine
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|thrust=180
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|isp-atm=275
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|isp-vac=305
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|vectoring=3
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|fuel=lfox
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}}
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{{Infobox/Part/test subject
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|environments=127
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|event=y
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|staging=y
 
}}
 
}}
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{{clear|right}}
 
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{{Infobox/Part/JetEngine
 
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|file=Rapier_Engine_01.png
 
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|manufacturer=C7 Aerospace Division and Rockmax Conglomerate
 
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|size=s
 
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|costs=5900
 
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|mass=1.75
 
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|drag=0.2
 
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|temp=3600
 
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|tolerance=20
 
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|thrust=190
 
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|fuel=0.3023
 
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|vectoring=3
 
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|since=0.23
 
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|part=rapierEngine
 
 
}}
 
}}

Latest revision as of 20:13, 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).
CR-7 R.A.P.I.E.R. Engine
Part image
Hybrid engine by
C7 Aerospace Divisionand Rockomax Conglomerate
Radial size Small
Cost (total) 6 000.00 Funds
Mass (total) 2.000 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 20 m/s
Research Aerospace tech.png Aerospace Tech
Unlock cost 35 000 Funds
Since version 0.23
Part configuration rapierEngine.cfg
Maximum thrust 105.00 kN
Isp (max) 3200 s
Fuel consumption 0.67 Units of fuel/s
Intake air consumption 4.02 Air unit/s
Thrust vectoring 3 °
Maximum thrust (1 atm) 162.30 kN
(vacuum) 180.00 kN
Isp (1 atm) 275 s
(vacuum) 305 s
Fuel consumption 12.04 Units of fuel/s
Thrust vectoring 3 °
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
Retrieved from "https://wiki.kerbalspaceprogram.com/index.php?title=CR-7_R.A.P.I.E.R._Engine/Box&oldid=108110"