Difference between revisions of "Template:Stats Table Solid Fuel Boosters"

From Kerbal Space Program Wiki
Jump to: navigation, search
m (Space saving, Specific Impulse -> Isp, Burn Time (s) -> Burn (s))
(Added Cost, Drag, Max Temp, Tolerance, approximate Fuel Density. Defined column width for better compatibility with various monitor aspect ratios and general neatness.)
Line 1: Line 1:
{| class="wikitable sortable"
+
{| class="wikitable sortable" style=white-space:nowrap
 
|-
 
|-
!colspan=4|
+
!colspan=4| {{#switch:{{{1}}}
 +
|=''Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron 1 is 31831 kg/m3)''
 +
|ru=''Плотность твердого топлива 1273-1910 кг/м3''
 +
|#default=''Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron 1 fuel density is 31831 kg/m3)''
 +
}}
 
!colspan=2| {{#switch:{{{1}}}
 
!colspan=2| {{#switch:{{{1}}}
|=Mass (t)
+
|=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]]
|ru=Масса (t)
+
|ru=[[wikipedia:ru:Масса|Масса]] [[wikipedia:ru:Тонна|(t)]]
|#default=Mass (t)
+
|#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]]
 
}}
 
}}
 +
!colspan=4|
 
!colspan=2| {{#switch:{{{1}}}
 
!colspan=2| {{#switch:{{{1}}}
|=T/W Ratio
+
|=[[w:Thrust-to-weight_ratio|T/W ratio]]
|ru=Тяга/Масса соотношение
+
|ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]]
|#default=T/W Ratio
+
|#default=[[w:Thrust-to-weight_ratio|T/W ratio]]
 
}}
 
}}
 
!colspan=2|
 
!colspan=2|
 
|-
 
|-
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
 
|=Image
 
|=Image
 
|ru=Вид
 
|ru=Вид
 
|#default=Image
 
|#default=Image
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="256px" | {{#switch:{{{1}}}
 
|=Part
 
|=Part
 
|ru=Название
 
|ru=Название
 
|#default=Part
 
|#default=Part
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="80px" | {{#switch:{{{1}}}
|=Radial Size
+
|=Size
|ru=Крепление
+
|ru=Размер
|#default=Radial Size
+
|#default=Size
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
|=Thrust (kN)
+
|=Cost ($)
|ru=Тяга (кН)
+
|ru=Цена ($)
|#default=Thrust (kN)
+
|#default=Cost ($)
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
 
|=Full
 
|=Full
 
|ru=Полный
 
|ru=Полный
 
|#default=Full
 
|#default=Full
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
 
|=Empty
 
|=Empty
 
|ru=Пустой
 
|ru=Пустой
 
|#default=Empty
 
|#default=Empty
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=[[w:Drag_(physics)|Drag]]
 +
|ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]]
 +
|#default=[[w:Drag_(physics)|Drag]]
 +
}}
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=Max Temp [[w:Kelvin|(K)]]
 +
|ru=максимальная температура [[wikipedia:ru:Кельвин|(K)]]
 +
|#default=Max Temp [[w:Kelvin|(K)]]
 +
}}
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=Tolerance
 +
|ru=целостность конструкции
 +
|#default=Tolerance
 +
}}
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=Thrust [[w:Newton_(unit)|(kN)]]
 +
|ru=Тяга [[wikipedia:ru:Ньютон_(единица_измерения)|(кН)]]
 +
|#default=Thrust [[w:Newton_(unit)|(kN)]]
 +
}}
 +
 
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 
|=Full
 
|=Full
 
|ru=Полный
 
|ru=Полный
 
|#default=Full
 
|#default=Full
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
 
|=Empty
 
|=Empty
 
|ru=Пустой
 
|ru=Пустой
 
|#default=Empty
 
|#default=Empty
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
|=Burn (s)
+
|=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
|ru=Время горения (с)
+
|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время горения]] [[wikipedia:ru:Секунда|(с)]]
|#default=Burn (s)
+
|#default=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
 
}}
 
}}
! {{#switch:{{{1}}}
+
! scope="col" width="60px" | {{#switch:{{{1}}}
|=Isp (s)
+
|=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
|ru=Удельный импульс (с)
+
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]
|#default=Isp (s)
+
|#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
 
}}
 
}}
 
|-
 
|-
Line 72: Line 98:
 
|#default=Small
 
|#default=Small
 
}}
 
}}
| 250
+
| 450
 
| 3.5
 
| 3.5
 
| 0.5
 
| 0.5
 +
| 0.3
 +
| 3600
 +
| 7
 +
| 250
 
| 7.3
 
| 7.3
 
| 51.0
 
| 51.0
Line 87: Line 117:
 
|#default=Small
 
|#default=Small
 
}}
 
}}
| 550
+
| 800
 
| 6.75
 
| 6.75
 
| 0.75
 
| 0.75
 +
| 0.3
 +
| 3900
 +
| 7
 +
| 550
 
| 7.6
 
| 7.6
 
| 68.0
 
| 68.0
Line 102: Line 136:
 
|#default=Radial Mounted
 
|#default=Radial Mounted
 
}}
 
}}
| 20
+
| 100
 
| 0.15
 
| 0.15
 
| 0.05
 
| 0.05
 +
| 0.3
 +
| 3600
 +
| 7
 +
| 20
 
| 13.6
 
| 13.6
 
| 40.8
 
| 40.8

Revision as of 20:11, 27 October 2012

Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron 1 fuel density is 31831 kg/m3) Mass (t) T/W ratio
Image Part Size Cost ($) Full Empty Drag Max Temp (K) Tolerance Thrust (kN) Full Empty Burn (s) Isp (s)
File:Rt-10 booster-t.png RT-10 Solid Fuel Booster Small 450 3.5 0.5 0.3 3600 7 250 7.3 51.0 25 212
File:Rt-b20 booster-t.png Rockomax BACC Solid Fuel Booster Small 800 6.75 0.75 0.3 3900 7 550 7.6 68.0 30 280
File:Sepratron 1.PNG Sepratron 1 Radial Mounted 100 0.15 0.05 0.3 3600 7 20 13.6 40.8 5 102