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

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== Trivia ==
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The Juno may be named after the [https://en.wikipedia.org/wiki/Junkers_Jumo_004| Junkers Jumo 004], one of the first jet engines.
 
== Changes ==
 
== Changes ==
 
;[[1.0.5]]
 
;[[1.0.5]]

Revision as of 18:44, 25 January 2016

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
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Usage

The J-20 "Juno" Basic Jet Engine is a simple air-breathing engine without many of the defining traits of the other jet engines. Its tiny (Mk0) size makes it useful for fuselage-mounted engines when used with the Mk0 Liquid Fuel Fuselage and the Small Circular Intake. Note that there are no aerodynamically-shaped command pods which share the same Mk0 size as the J-20, however many Probodobodyne Inc. cores have the same general diameter.

Visualization of the thrust multiplier curve for velocity
Visualization of the thrust multiplier curve for atmospheric pressure

Product description

A small turbojet. Not very efficient, anemic thrust, but hey--it's cheap! And it's so cute...look at the little thing!

Trivia

The Juno may be named after the Junkers Jumo 004, one of the first jet engines.

Changes

1.0.5
  • Initial release