Difference between revisions of "J-X4 "Whiplash" Turbo Ramjet Engine/Box"

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<noinclude>{{Data template used}}</noinclude>{{Infobox/Part
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<noinclude>{{Data template used}}</noinclude>
|file=turbojetengine.png
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{{Infobox/Part
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|file=JX4WhiplashTurboRamjetEngine.png
 
|type=je
 
|type=je
 
|size=s
 
|size=s
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|temp=2000
 
|temp=2000
 
|tolerance=7
 
|tolerance=7
|research=High Altitude Flight
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|research=Hypersonic Flight
 
|unlock cost=18000
 
|unlock cost=18000
 
|since=0.15
 
|since=0.15
 
|filename=jetEngineTurbo.cfg
 
|filename=jetEngineTurbo.cfg
 
|part=jetEngineTurbo
 
|part=jetEngineTurbo
|more=
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|more={{Infobox/Part/title|je}}
 
{{Infobox/Part/jet engine
 
{{Infobox/Part/jet engine
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|intake=8 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) -->
 
|isp=4000
 
|isp=4000
 
|thrust=130
 
|thrust=130
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}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=71
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|environments=31
 
|event=True
 
|event=True
 
|staging=True
 
|staging=True
 
}}
 
}}
 
}}
 
}}

Latest revision as of 11:25, 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-X4 "Whiplash" Turbo Ramjet Engine
Part image
Jet engine by
C7 Aerospace Division

Radial size Small
Cost (total) 2 250.00 Funds
Mass (total) 1.80 t
Drag 0.2
Max. Temp. 2000 K
Volume  ?
Impact Tolerance 7 m/s
Research Hypersonic flight.png Hypersonic Flight
Unlock cost 18 000 Funds
Since version 0.15
Part configuration jetEngineTurbo.cfg
Jet engine
Maximum thrust 130 kN
Isp (max) 4000 s
Fuel consumption 0.66 Units of fuel/s
Intake air consumption 5.30 Air unit/s
Thrust vectoring 1 °
Testing Environments
On the surface Yes
In the ocean Yes
On the launchpad Yes
In the atmosphere Yes
Sub orbital Yes
In an orbit No
On an escape No
Docked No
Test by staging Yes
Manually testable Yes