Difference between revisions of "Template:Stats Table Escape Systems"
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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 | + | | [[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 (  )
|
Thrust (kN) |
TWR | Isp (s) | Burn (s) | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Full | Empty | |||||||||||||||||
| Image | Part | Radial size | Cost (  ) |
Full | Empty | Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
atm | vac | atm | vac | atm | vac | atm | vac | ||
 |
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 |
