Difference between revisions of "Structural Pylon/Box"
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|type=dec | |type=dec | ||
|manufacturer=C7 | |manufacturer=C7 | ||
− | |costs= | + | |costs=125 |
|mass=0.2 | |mass=0.2 | ||
|drag=0.2 | |drag=0.2 | ||
− | |temp= | + | |temp=2000 |
− | |tolerance= | + | |tolerance=70 |
− | |research= | + | |research=High Altitude Flight |
+ | |unlock cost=6800 | ||
|since=0.15 | |since=0.15 | ||
+ | |filename=structuralPylon.cfg | ||
|part=structuralPylon | |part=structuralPylon | ||
+ | |parent=Structural | ||
|more={{Infobox/Part/separator | |more={{Infobox/Part/separator | ||
− | |ejection= | + | |ejection=250 |
+ | }} | ||
+ | {{Infobox/Part/test subject | ||
+ | |environments=15 | ||
+ | |event=False | ||
+ | |staging=True | ||
}} | }} | ||
}} | }} |
Latest revision as of 10:32, 18 January 2016
Structural Pylon | ||
Decoupler by C7 Aerospace Division | ||
Cost | (total) | 125.00 |
Mass | (total) | 0.20 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Volume | ? | |
Impact Tolerance | 70 m/s | |
Research | High Altitude Flight | |
Unlock cost | 6 800 | |
Since version | 0.15 | |
Part configuration | structuralPylon.cfg | |
Ejection momentum | 2500 Ns | |
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 | No |