Difference between revisions of "J-20 "Juno" Basic Jet Engine"
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| + | {{:J-20 "Juno" Basic Jet Engine/Box}} | ||
| + | {{Stub}} | ||
| + | == Usage == | ||
| + | [[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]] | ||
| + | |||
== Product description == | == Product description == | ||
{{Quote | {{Quote | ||
|A small turbojet. Not very efficient, anemic thrust, but hey--it's cheap! And it's so cute...look at the little thing! | |A small turbojet. Not very efficient, anemic thrust, but hey--it's cheap! And it's so cute...look at the little thing! | ||
}} | }} | ||
| − | |||
| − | |||
== Changes == | == Changes == | ||
Revision as of 05:21, 26 November 2015
| 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 | |
Usage
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! | ” |
Changes
- Initial release
