Difference between revisions of "Sepratron I/Box"

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m (*update to 0.24.2;)
m (*update to 0.25;)
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|costs=50
 
|costs=50
 
|mass=0.0125
 
|mass=0.0125
|sf=8
+
|sf=8.000
 
|drag=0.2-0.3
 
|drag=0.2-0.3
 
|temp=3600
 
|temp=3600
 
|tolerance=7
 
|tolerance=7
 
|research=General Rocketry
 
|research=General Rocketry
 +
|unlock cost=1100
 
|since=0.17
 
|since=0.17
|part=sepMotor1
+
|filename=solidBoosterSep.cfg
 +
|part=solidBoosterSep
 
|more={{Infobox/Part/solid fuel engine
 
|more={{Infobox/Part/solid fuel engine
 
|thrust=18
 
|thrust=18
|fuel=8
 
 
|isp-atm=100
 
|isp-atm=100
 
|isp-vac=100
 
|isp-vac=100
 +
|fuel=8.0
 +
}}
 +
{{Infobox/Part/test subject
 +
|environments=15
 +
|staging=True
 +
|event=False
 
}}
 
}}
 
}}
 
}}

Revision as of 01:35, 8 October 2014

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) 50.00 Funds
(dry) 45.20 Funds
Mass (total) 0.073 t
(dry) 0.013 t
Drag 0.2-0.3
Max. Temp. 3600 K
Impact Tolerance 7 m/s
Research General rocketry.png General Rocketry
Unlock cost 1 100 Funds
Since version 0.17
Part configuration solidBoosterSep.cfg
Maximum thrust (1 atm) 18.00 kN
(vacuum) 18.00 kN
Isp (1 atm) 100 s
(vacuum) 100 s
Fuel consumption 2.45 Units of fuel/s
Thrust vectoring No
Burn time (1 atm) 3.3 s
(vacuum) 3.3 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 No