Difference between revisions of "Sepratron I/Box"

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m (*update to 1.0.2;)
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|costs=75
 
|costs=75
 
|mass=0.0125
 
|mass=0.0125
|sf=8.000
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|sf=8
 
|drag=0.2-0.3
 
|drag=0.2-0.3
 
|temp=2000
 
|temp=2000
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|filename=solidBoosterSep.cfg
 
|filename=solidBoosterSep.cfg
 
|part=solidBoosterSep
 
|part=solidBoosterSep
 +
|parent=Engine
 
|more={{Infobox/Part/solid fuel engine
 
|more={{Infobox/Part/solid fuel engine
|fuel=8.0
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|thrust=18
|isp-atm=118
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|isp-atm=118
|isp-vac=154
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|isp-vac=154
|thrust=18
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|fuel=8
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
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|environments=60
|event=False
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|event=y
|staging=True
+
|staging=y
 +
}}
 +
{{Infobox/Part/cargo
 +
|volume=25
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|stack=2
 +
}}
 +
{{Infobox/Part/tank
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|sf=8
 
}}
 
}}
 
}}
 
}}

Latest revision as of 20:28, 9 October 2024

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
Sepratron I
Part image
Solid rocket booster by
Periapsis Rocket Supplies Co

Radial size Radial mounted
Cost (total) 75.00 Funds
(dry) 70.20 Funds
Mass (total) 0.073 t
(dry) 0.013 t
Drag 0.2-0.3
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Precision propulsion.png Precision Propulsion
Unlock cost 1 100 Funds
Since version 0.17
Part configuration solidBoosterSep.cfg
Maximum thrust (1 atm) 13.79 kN
(vacuum) 18.00 kN
Isp (1 atm) 118 s
(vacuum) 154 s
Fuel consumption 1.59 Units of fuel/s
Thrust vectoring No
Burn time (1 atm) 3.9 s
(vacuum) 5 s
Testing Environments
On the surface No
In the ocean No
On the launchpad Yes
In the atmosphere Yes
Sub-orbital Yes
In an orbit Yes
On an escape No
Docked No
Test by staging Yes
Manually testable Yes
Packed volume 25 l
Stacking capacity 2 units
Solid fuel 8 Units of fuel