Difference between revisions of "Mk1 Liquid Fuel Fuselage"
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UmbralRaptor (talk | contribs) (version info, phrasing, diameter.) |
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− | The '''Mk1 Fuselage''' is a round cylindrical fuselage part with a diameter of 1 | + | The '''Mk1 Fuselage''' is a round cylindrical fuselage part with a diameter of 1.25 meters. It contains only [[liquid fuel]]. It is not to be confused by the [[Structural Fuselage]] that cannot store fuel. |
== Description == | == Description == | ||
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== Comparisons == | == Comparisons == | ||
− | This is the least-efficient by weight of all the fuselages: its | + | This is the least-efficient by weight of all the fuselages: its mass ratio is only 3.14, with all the others (as of .20.2) have a ratio of 5. |
+ | |||
== Changes == | == Changes == | ||
− | ; | + | ;{{Version|0.15|}} |
+ | * Dry mass increased from 0.3 to 0.35, fuel system changes reduced full mass from 1.2 to 1.1. | ||
+ | ;{{Version|0.15|}} | ||
* Initial release | * Initial release | ||
{{Parts}} | {{Parts}} |
Revision as of 21:11, 18 July 2013
Mk1 Liquid Fuel Fuselage | ||
Liquid fuel tank by C7 Aerospace Division | ||
Radial size | Small, Radial mounted | |
Cost | (total) | 550.00 |
(dry) | 230.00 | |
Mass | (total) | 2.25 t |
(dry) | 0.25 t | |
Drag | 0.3-0.2 | |
Max. Temp. | 2000 K | |
Volume | ? | |
Impact Tolerance | 10 m/s | |
Research | Aviation | |
Unlock cost | 2 600 | |
Since version | 0.15 | |
Part configuration | mk1Fuselage.cfg | |
Liquid fuel | 400 |
The Mk1 Fuselage is a round cylindrical fuselage part with a diameter of 1.25 meters. It contains only liquid fuel. It is not to be confused by the Structural Fuselage that cannot store fuel.
Description
“ | A standard fuselage that carries fuel for spaceplanes. This one is chock-full of jet fuel. Not as resistant as it's counterparts, but jet fuel is more efficient than the other fuels, without mentioning lighter. — C7 Aerospace Division |
” |
Comparisons
This is the least-efficient by weight of all the fuselages: its mass ratio is only 3.14, with all the others (as of .20.2) have a ratio of 5.
Changes
- Dry mass increased from 0.3 to 0.35, fuel system changes reduced full mass from 1.2 to 1.1.
- Initial release