Difference between revisions of "Sepratron I/Box"

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m (image update)
(*update to module system; +data template note; +research node; !mass;)
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{{Infobox/Part/Engine/Solid
+
<noinclude>{{Data template used}}</noinclude>
 +
{{Infobox/Part
 
|file=Sepratron.png
 
|file=Sepratron.png
 +
|type=srb
 
|manufacturer=PeRS
 
|manufacturer=PeRS
 
|size=r
 
|size=r
 
|costs=100
 
|costs=100
|mass=0.0725
+
|mass=0.0125
 +
|sf=8
 
|drag=0.3
 
|drag=0.3
 
|temp=3600
 
|temp=3600
 
|tolerance=7
 
|tolerance=7
 +
|research=General Rocketry
 +
|since=0.17
 +
|part=sepMotor1
 +
|more={{Infobox/Part/solid fuel engine
 
|thrust=18
 
|thrust=18
 
|fuel=8
 
|fuel=8
 
|isp-atm=100
 
|isp-atm=100
 
|isp-vac=100
 
|isp-vac=100
|since=0.17
+
}}
|part=sepMotor1
 
 
}}
 
}}

Revision as of 11:24, 11 February 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) 100.00 Funds
(dry) 95.20 Funds
Mass (total) 0.07250 t
(dry) 0.01250 t
Drag 0.3
Max. Temp. 3600 K
Volume  ?
Impact Tolerance 7 m/s
Research General rocketry.png General Rocketry
Unlock cost 0 Funds
Since version 0.17
Part configuration [[Parts/Engine/sepMotor1/{{{filename}}}|{{{filename}}}]]
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
Fuel Units of fuel
Burn time (1 atm) 3.3 s
(vacuum) 3.3 s