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
+
|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) 0.073 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 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