Difference between revisions of "Template:Stats Table Escape Systems"

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(Create table for LES)
 
(Localized using Dict/part name)
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! colspan=4 rowspan=2 | ''{{lang
 
! colspan=4 rowspan=2 | ''{{lang
 
|en=Solid Fuel Density is 7.5 kg/unit
 
|en=Solid Fuel Density is 7.5 kg/unit
 +
|fr=La densité de l'ergol solide est de 7.5 kg/unité
 
|ru=Плотность твердого топлива 7,5 кг/ед.
 
|ru=Плотность твердого топлива 7,5 кг/ед.
 
|pl=Gęstość paliwa stałego wynosi 7500 kg/m3 - (W przypadku Sepratron I to 7500 kg/m3)
 
|pl=Gęstość paliwa stałego wynosi 7500 kg/m3 - (W przypadku Sepratron I to 7500 kg/m3)
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! rowspan=3 | {{lang
 
! rowspan=3 | {{lang
 
|en=[[Solid fuel|Fuel]]<br>{{nowrap|({{Mark|fuelu}})}}
 
|en=[[Solid fuel|Fuel]]<br>{{nowrap|({{Mark|fuelu}})}}
 +
|fr=[[Solid fuel/fr|Ergol]]<br>{{nowrap|({{Mark|fuelu}})}}
 
|ru=Запас<br>[[Solid fuel/ru|топлива]]<br>{{nowrap|({{Mark|fuelu}})}}
 
|ru=Запас<br>[[Solid fuel/ru|топлива]]<br>{{nowrap|({{Mark|fuelu}})}}
 
|pl=Paliwo<br>{{nowrap|({{Mark|fuelu}})}}
 
|pl=Paliwo<br>{{nowrap|({{Mark|fuelu}})}}
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! rowspan=3 | {{lang
 
! rowspan=3 | {{lang
 
|en=[[w:Solid-fuel_rocket|Burn]]<br>[[w:Second|(s)]]
 
|en=[[w:Solid-fuel_rocket|Burn]]<br>[[w:Second|(s)]]
 +
|fr=Durée de fonctionnement<br>[[w:fr:Seconde|(s)]]
 
|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время<br>горения]]<br>[[wikipedia:ru:Секунда|(с)]]
 
|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время<br>горения]]<br>[[wikipedia:ru:Секунда|(с)]]
 
|pl=[[w:pl:Rakieta na paliwo stałe|Spalanie]]<br>[[w:pl:Sekunda|(s)]]
 
|pl=[[w:pl:Rakieta na paliwo stałe|Spalanie]]<br>[[w:pl:Sekunda|(s)]]
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|-
 
|-
 
| {{SortCell|1}}[[File:Launch_Escape_System.png|60x60px|center]]
 
| {{SortCell|1}}[[File:Launch_Escape_System.png|60x60px|center]]
| {{if lang link|Launch Escape System|hu=Menőrakéta <br> [Launch Escape System]|ru=Система Аварийного Спасения<br>(Launch Escape System)|ko=비상 탈출 시스템(Launch Escape System)}}
+
| [[Launch Escape System{{if lang}}|{{Dict/part name|Launch Escape System}}]]
 
{{Radial Size/Cell|1}}
 
{{Radial Size/Cell|1}}
 
| {{Formatnum/SortCell|1000}}<br>(982)
 
| {{Formatnum/SortCell|1000}}<br>(982)

Revision as of 16:58, 9 June 2019

Solid Fuel Density is 7.5 kg/unit Mass
(t)
Fuel
(Units of fuel)
Thrust
(kN)
TWR Isp (s) Burn
(s)
Full Empty
Image Part Radial size Cost
(Funds)
Full Empty Max. Temp.
(K)
Tolerance
(m/s)
Tolerance
(g)
atm vac atm vac atm vac atm vac
Launch Escape System.png
Launch Escape System Small 1 000
(982)
1.125 0.90 2 700 15 50 30 666.67 750.0 60.43 67.98 75.53 84.98 160 180 0.5