Difference between revisions of "J-90 "Goliath" Turbofan Engine"
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The '''J-90 "Goliath" Turbofan Engine''' is a [[jet engine]] added with version 1.0.5 of Kerbal Space Program. | The '''J-90 "Goliath" Turbofan Engine''' is a [[jet engine]] added with version 1.0.5 of Kerbal Space Program. | ||
+ | == Usage == | ||
+ | [[File:J-90 Goliath Turbofan Engine velocity curve.png|thumb|Visualization of the thrust multiplier curve for velocity]] | ||
+ | [[File:J-90 Goliath Turbofan Engine atmosphere curve.png|thumb|Visualization of the thrust multiplier curve for atmospheric pressure]] | ||
== Product description == | == Product description == | ||
{{Quote|A high performance jet engine with a variable geometry thrust vectoring nozzle and an afterburner for extra thrust.|C7 Aerospace Division}} | {{Quote|A high performance jet engine with a variable geometry thrust vectoring nozzle and an afterburner for extra thrust.|C7 Aerospace Division}} |
Revision as of 05:24, 26 November 2015
J-90 "Goliath" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Radial size | Radial mounted | |
Cost | (total) | 2 600.00 |
(dry) | 2 600.00 | |
Mass | (total) | 4.517 t |
(dry) | 4.517 t | |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Impact Tolerance | 7 m/s | |
Research | Heavy Aerodynamics | |
Unlock cost | 15 000 | |
Since version | 1.0.5 | |
Part configuration | jetEngineBig.cfg | |
Intake speed | 30 m/s | |
Intake area | 3 m2 | |
Maximum thrust | 360.00 kN | |
Isp | (max) | 12600 s |
Fuel consumption | 0.58 /s | |
Intake air consumption | 132.27 /s | |
Thrust vectoring | No | |
Electricity generated | 16 ⚡/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 | |
Intake air | 3 |
The J-90 "Goliath" Turbofan Engine is a jet engine added with version 1.0.5 of Kerbal Space Program.
Usage
Product description
“ | A high performance jet engine with a variable geometry thrust vectoring nozzle and an afterburner for extra thrust. — C7 Aerospace Division |
” |
Changes
- Initial release