Difference between revisions of "Sepratron I/Box"

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m (*update to 0.25;)
m (*update to 1.0;)
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|size=r
 
|size=r
 
|manufacturer=PeRS
 
|manufacturer=PeRS
|costs=50
+
|costs=75
 
|mass=0.0125
 
|mass=0.0125
 
|sf=8.000
 
|sf=8.000
 
|drag=0.2-0.3
 
|drag=0.2-0.3
|temp=3600
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|temp=2000
 
|tolerance=7
 
|tolerance=7
|research=General Rocketry
+
|research=Precision Propulsion
 
|unlock cost=1100
 
|unlock cost=1100
 
|since=0.17
 
|since=0.17
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|more={{Infobox/Part/solid fuel engine
 
|more={{Infobox/Part/solid fuel engine
 
|thrust=18
 
|thrust=18
|isp-atm=100
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|isp-atm=118
|isp-vac=100
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|isp-vac=154
 
|fuel=8.0
 
|fuel=8.0
 
}}
 
}}

Revision as of 17:12, 29 April 2015

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) 0.07250 t
(dry) 0.01250 t
Drag 0.2-0.3
Max. Temp. 2000 K
Volume  ?
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
Fuel 8.0 Units of fuel
Burn time (1 atm) 3.9 s
(vacuum) 5 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