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

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{{Infobox/Part
 
{{Infobox/Part
 
|file=Rapier Engine_01.png
 
|file=Rapier Engine_01.png
|role={{lang|en=Hybrid engine|pl=Silnik hybrydowy}}
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|type=he
|size=s
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|size=1
 
|manufacturer=C7
 
|manufacturer=C7
 
|manufacturer2=RMC
 
|manufacturer2=RMC
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|part=rapierEngine
 
|part=rapierEngine
 
|parent=Engine
 
|parent=Engine
|more=
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|more={{Infobox/Part/jet engine
{{Infobox/Part/title|lfe}}
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|thrust=105
 +
|isp=3200
 +
|vectoring=3
 +
|intake=6
 +
}}
 
{{Infobox/Part/reaction engine
 
{{Infobox/Part/reaction engine
|fuel=lfox
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|thrust=180
|isp-atm=275
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|isp-atm=275
|isp-vac=305
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|isp-vac=305
|thrust=180
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|vectoring=3
|vectoring=3
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|fuel=lfox
}}
 
{{Infobox/Part/title|je}}
 
{{Infobox/Part/jet engine
 
|intake=6
 
|isp=3200
 
|thrust=105
 
|vectoring=3
 
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=127
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|environments=127
|event=True
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|event=y
|staging=True
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|staging=y
 
}}
 
}}
 
}}
 
}}

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