Difference between revisions of "Sepratron I/Box"

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{{Infobox/Part/Engine/Solid
+
<noinclude>{{Data template used}}</noinclude>
 +
{{Infobox/Part
 
|file=Sepratron.png
 
|file=Sepratron.png
 +
|type=srb
 +
|size=r
 
|manufacturer=PeRS
 
|manufacturer=PeRS
|size=r
+
|costs=75
|costs=100
+
|mass=0.0125
|mass=0.0725
+
|sf=8.000
|drag=0.3
+
|drag=0.2-0.3
|temp=3600
+
|temp=2000
 
|tolerance=7
 
|tolerance=7
 +
|research=Precision Propulsion
 +
|unlock cost=1100
 +
|since=0.17
 +
|filename=solidBoosterSep.cfg
 +
|part=solidBoosterSep
 +
|more={{Infobox/Part/title|srb}}
 +
{{Infobox/Part/solid fuel engine
 +
|fuel=8.0
 +
|isp-atm=118
 +
|isp-vac=154
 
|thrust=18
 
|thrust=18
|fuel=8
+
}}
|isp-atm=100
+
{{Infobox/Part/test subject
|isp-vac=100
+
|environments=60
|since=0.17
+
|event=True
|part=sepMotor1
+
|staging=True
 +
}}
 
}}
 
}}

Latest revision as of 11:00, 18 August 2018

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
Solid rocket booster
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