Difference between revisions of "J-20 "Juno" Basic Jet Engine/Box"

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|file=J90JunoBasicJetEngine.png
 
|file=J90JunoBasicJetEngine.png
 
|type=je
 
|type=je
|size=t
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|size=0
 
|manufacturer=C7
 
|manufacturer=C7
 
|costs=450
 
|costs=450
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|unlock cost=2000
 
|unlock cost=2000
 
|since=1.0.5
 
|since=1.0.5
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|filename=SmallJetEngine.cfg
 
|part=miniJet
 
|part=miniJet
|filename=SmallJetEngine.cfg
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|parent=Engine
|more={{Infobox/Part/title|je}}
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|more={{Infobox/Part/jet engine
{{Infobox/Part/jet engine
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|thrust=20
|intake=22 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) -->
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|isp=6400
|isp=6400
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|intake=22
|thrust=20
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}}
|vectoring=
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{{Infobox/Part/generator
 +
|generate=1
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
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|environments=15
|event=True
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|event=y
|staging=True
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|staging=y
 +
}}
 +
{{Infobox/Part/cargo
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|volume=220
 
}}
 
}}
 
}}
 
}}

Latest revision as of 20:14, 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).
J-20 "Juno" Basic Jet Engine
Part image
Jet engine by
C7 Aerospace Division

Radial size Tiny
Cost (total) 450.00 Funds
Mass (total) 0.250 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Aviation.png Aviation
Unlock cost 2 000 Funds
Since version 1.0.5
Part configuration SmallJetEngine.cfg
Maximum thrust 20.00 kN
Isp (max) 6400 s
Fuel consumption 0.06 Units of fuel/s
Intake air consumption 1.40 Air unit/s
Thrust vectoring No
Electricity generated 1 ⚡/s
Testing Environments
On the surface Yes
In the ocean Yes
On the launchpad Yes
In the atmosphere Yes
Sub-orbital No
In an orbit No
On an escape No
Docked No
Test by staging Yes
Manually testable Yes
Packed volume 220 l