Difference between revisions of "J-20 "Juno" Basic Jet Engine"
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== Usage == | == 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. | + | 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. This engine is not for impatient pilots, as its acceleration is minimal, especially on the bumpy level 1 [[runway]] in early [[career]] mode. |
[[File:J-20 Juno Basic Jet Engine velocity curve.png|thumb|Visualization of the thrust multiplier curve for velocity]] | [[File:J-20 Juno Basic Jet Engine velocity curve.png|thumb|Visualization of the thrust multiplier curve for velocity]] | ||
[[File:J-20 Juno Basic Jet Engine atmosphere curve.png|thumb|Visualization of the thrust multiplier curve for atmospheric pressure]] | [[File:J-20 Juno Basic Jet Engine atmosphere curve.png|thumb|Visualization of the thrust multiplier curve for atmospheric pressure]] |
Revision as of 22:03, 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 |
Contents
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. This engine is not for impatient pilots, as its acceleration is minimal, especially on the bumpy level 1 runway in early career mode.
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
- Initial release