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>
{{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
{{Infobox/Part/Engine/Liquid
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|file=Rapier Engine_01.png
|file=Rapier_Engine_01.png
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|type=he
|manufacturer=C7 Aerospace Division and Rockmax Conglomerate
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|size=1
|size=s
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|manufacturer=C7
|costs=5900
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|manufacturer2=RMC
|mass=1.75
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|costs=6000
 +
|mass=2.0
 
|drag=0.2
 
|drag=0.2
|temp=3600
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|temp=2000
 
|tolerance=20
 
|tolerance=20
|thrust=175
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|research=Aerospace Tech
|isp-atm=320
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|unlock cost=35000
|isp-vac=360
 
|vectoring=3
 
 
|since=0.23
 
|since=0.23
 +
|filename=rapierEngine.cfg
 
|part=rapierEngine
 
|part=rapierEngine
 +
|parent=Engine
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|more={{Infobox/Part/jet engine
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|thrust=105
 +
|isp=3200
 +
|vectoring=3
 +
|intake=6
 +
}}
 +
{{Infobox/Part/reaction engine
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|thrust=180
 +
|isp-atm=275
 +
|isp-vac=305
 +
|vectoring=3
 +
|fuel=lfox
 +
}}
 +
{{Infobox/Part/test subject
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|environments=127
 +
|event=y
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|staging=y
 
}}
 
}}
{{clear|right}}
 
{{Infobox/Part/JetEngine
 
|file=Rapier_Engine_01.png
 
|manufacturer=C7 Aerospace Division and Rockmax Conglomerate
 
|size=s
 
|costs=5900
 
|mass=1.75
 
|drag=0.2
 
|temp=3600
 
|tolerance=20
 
|thrust=190
 
|fuel=0.3023
 
|vectoring=3
 
|since=0.23
 
|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