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

Revision as of 21:55, 2 February 2016

J-20 "Juno" Basic Jet Engine
Jet engine by C7 Aerospace Division
Radial size		Tiny
Cost	(total)	450.00
Mass	(total)	0.250 t
Drag		0.2
Max. Temp.		2000 K
Impact Tolerance		7 m/s
Research		Aviation
Unlock cost		2 000
Since version		1.0.5
Part configuration		SmallJetEngine.cfg
Maximum thrust		20.00 kN
Isp	(max)	6400 s
Fuel consumption		0.06 /s
Intake air consumption		1.40 /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

Trivia

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

Changes

1.0.5

• Initial release