Difference between revisions of "Template:Stats Table Jet Engines"

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m (Space saving, Specific Impulse -> Isp)
(Added Cost, Drag, Max Temp, Tolerance, TVC, Gimbal, Optimal Airflow, Intake Size, Intake Power. Defined column width for better compatibility with various monitor aspect ratios and general neatness.)
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{| class="wikitable sortable"
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{| class="wikitable sortable" style=white-space:nowrap
 
|-
 
|-
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!colspan=7|
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!colspan=11|
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!colspan=2| {{#switch:{{{1}}}
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!colspan=1|{{#switch:{{{1}}}
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|=Isp (s)
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|=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
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|ru=Удельный импульс (с)
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|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]
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|#default=Isp (s)
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|#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
 
}}
 
}}
 
|-
 
|-
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}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="256px" | {{#switch:{{{1}}}
 
|=Part
 
|=Part
 
|ru=Название
 
|ru=Название
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}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="80px" | {{#switch:{{{1}}}
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|=Radial Size
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|=Size
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|ru=Крепление
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|ru=Размер
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|#default=Radial Size
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|#default=Size
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}}
 +
 
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Cost ($)
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|ru=Цена ($)
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|#default=Cost ($)
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}}
 +
 
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]]
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|ru=[[wikipedia:ru:Масса|Масса]] [[wikipedia:ru:Тонна|(t)]]
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|#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]]
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}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=[[w:Drag_(physics)|Drag]]
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|ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]]
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|#default=[[w:Drag_(physics)|Drag]]
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}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Max Temp [[w:Kelvin|(K)]]
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|ru=максимальная температура [[wikipedia:ru:Кельвин|(K)]]
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|#default=Max Temp [[w:Kelvin|(K)]]
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}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Tolerance
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|ru=целостность конструкции
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|#default=Tolerance
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}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Thrust [[w:Newton_(unit)|(kN)]]
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|ru=Тяга [[wikipedia:ru:Ньютон_(единица_измерения)|(кН)]]
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|#default=Thrust [[w:Newton_(unit)|(kN)]]
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}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=[[w:Thrust-to-weight_ratio|T/W ratio]]
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|ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]]
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|#default=[[w:Thrust-to-weight_ratio|T/W ratio]]
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}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]]
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|ru=[[wikipedia:ru:Ракетное_топливо|топливо]] [[wikipedia:ru:Расходомер|(L/s)]]
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|#default=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]]
 
}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Thrust (kN)
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|=[[w:Atmosphere_(unit)|atm]]
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|ru=Тяга (кН)
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|ru=[[wikipedia:ru:Атмосфера_(единица_измерения)|атм]]
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|#default=Thrust (kN)
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|#default=[[w:Atmosphere_(unit)|atm]]
 
}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Mass (t)
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|=[[w:Thrust_Vectoring|TVC]]
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|ru=Масса (t)
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|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]]
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|#default=Mass (t)
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|#default=[[w:Thrust_Vectoring|TVC]]
 
}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=T/W ratio
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|=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]]
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|ru=|ru=Тяга/Масса соотношение
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|ru=[[wikipedia:ru:Карданов_подвес|Карданов подвес]] [[wikipedia:ru:Градус_(геометрия)|(°)]]
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|#default=T/W ratio
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|#default=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]]
 
}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=Fuel (L/s)
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|=Opt. Airflow
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|ru=Потребление топлива (единиц/сек)
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|ru=Оптимальный воздушный поток
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|#default=Fuel (L/s)
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|#default=Opt. Airflow
 
}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=atm
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|=Int. Size
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|ru=атм
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|ru=Размер впускного
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|#default=atm
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|#default=Int. Size
 
}}
 
}}
  
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! {{#switch:{{{1}}}
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! scope="col" width="60px" | {{#switch:{{{1}}}
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|=vac
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|=Int. Power
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|ru=вак
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|ru=Впускной питания
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|#default=vac
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|#default=Int. Power
 
}}
 
}}
  
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|#default=Small
 
|#default=Small
 
}}
 
}}
 +
| 950
 +
| 1
 +
| 0.2
 +
| 3600
 +
| 7
 
| 100
 
| 100
−
| 1
 
 
| 10.2
 
| 10.2
 
| 0.3
 
| 0.3
−
| 1456 <sub>stall</sub> - 7282 <sub>max</sub>  
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| 1456 <sub>stall</sub> - 7282 <sub>max</sub>
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| 0
+
| Yes
 +
| 2.5
 +
| 200
 +
| 1.1
 +
| 125
 
|-
 
|-
 
| [[Image:Turbojet-t.png|60x60px|]]
 
| [[Image:Turbojet-t.png|60x60px|]]
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|#default=Small
 
|#default=Small
 
}}
 
}}
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| 950
 +
| 1.2
 +
| 0.2
 +
| 3600
 +
| 7
 
| 150
 
| 150
−
| 1.2
 
 
| 12.7
 
| 12.7
 
| 0.4
 
| 0.4
 
| 546 <sub>stall</sub> - 8192 <sub>max</sub>  
 
| 546 <sub>stall</sub> - 8192 <sub>max</sub>  
−
| 0
+
| Yes
 +
| 2.5
 +
| 60
 +
| 1.0
 +
| 200
 
|-
 
|-
 
|}
 
|}

Revision as of 22:09, 27 October 2012

Isp (s)
Image Part Size Cost ($) Mass (t) Drag Max Temp (K) Tolerance Thrust (kN) T/W ratio Fuel (L/s) atm TVC Gimbal (°) Opt. Airflow Int. Size Int. Power
File:Basic jet engine-t.png Basic Jet Engine Small 950 1 0.2 3600 7 100 10.2 0.3 1456 stall - 7282 max Yes 2.5 200 1.1 125
File:Turbojet-t.png TurboJet Engine Small 950 1.2 0.2 3600 7 150 12.7 0.4 546 stall - 8192 max Yes 2.5 60 1.0 200
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