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

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(+applied reaction engine module;)
m (Update part)
 
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{{Infobox/Part
 
{{Infobox/Part
 
|file=Rapier Engine_01.png
 
|file=Rapier Engine_01.png
|role=Hybrid engine
+
|type=he
|parent=Engine
+
|size=1
|manufacturer=C7 Aerospace Division
+
|manufacturer=C7
|manufacturer2=Rockmax Conglomerate
+
|manufacturer2=RMC
|size=s
+
|costs=6000
|costs=5900
+
|mass=2.0
|mass=1.75
 
 
|drag=0.2
 
|drag=0.2
|temp=3600
+
|temp=2000
 
|tolerance=20
 
|tolerance=20
|research=Hypersonic Flight
+
|research=Aerospace Tech
 +
|unlock cost=35000
 
|since=0.23
 
|since=0.23
 +
|filename=rapierEngine.cfg
 
|part=rapierEngine
 
|part=rapierEngine
|more=
+
|parent=Engine
{{Infobox/Line|'''Liquid fuel engine'''|style=text-align:center;text-decoration:underline;}}
+
|more={{Infobox/Part/jet engine
 +
|thrust=105
 +
|isp=3200
 +
|vectoring=3
 +
|intake=6
 +
}}
 
{{Infobox/Part/reaction engine
 
{{Infobox/Part/reaction engine
|thrust=175
+
|thrust=180
|isp-atm=320
+
|isp-atm=275
|isp-vac=360
+
|isp-vac=305
|vectoring=3
+
|vectoring=3
 +
|fuel=lfox
 
}}
 
}}
{{Infobox/Line|'''Jet engine'''|style=text-align:center;text-decoration:underline;}}
+
{{Infobox/Part/test subject
{{Infobox/Part/JetEngine
+
|environments=127
|thrust=190
+
|event=y
|stall=63 (?)
+
|staging=y
|isp=800
 
|vectoring=3
 
 
}}
 
}}
 
}}
 
}}

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