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

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{{Infobox/Part/jet engine
 
|intake=22 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) -->
 
|intake=22 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) -->
 
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Revision as of 11:24, 18 August 2018

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
Jet engine
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
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