Difference between revisions of "Template:Stats Table RCS Thrusters"
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! scope="col" width="50px" | {{lang | ! scope="col" width="50px" | {{lang | ||
|en=[[Monopropellant|Fuel]]<br>({{Mark|fuelflow}}) | |en=[[Monopropellant|Fuel]]<br>({{Mark|fuelflow}}) | ||
+ | |fr=[[Monopropellant/fr|Ergol]]<br>({{Mark|fuelflow}}) | ||
|ja=[[Monopropellant/ja|燃料]]<br>({{Mark|fuelflow}}) | |ja=[[Monopropellant/ja|燃料]]<br>({{Mark|fuelflow}}) | ||
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| {{SortCell|1}}[[File:RV-105.png|60x60px|center]] | | {{SortCell|1}}[[File:RV-105.png|60x60px|center]] | ||
− | | | + | | [[RV-105 RCS Thruster Block{{if lang}}|{{Dict/part name|RV-105 RCS Thruster Block}}]] |
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{{Radial Size/Cell|r}} | {{Radial Size/Cell|r}} | ||
| {{Formatnum/SortCell|45}} | | {{Formatnum/SortCell|45}} | ||
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| {{SortCell|2}}[[File:Linear RCS.png|60x60px|center]] | | {{SortCell|2}}[[File:Linear RCS.png|60x60px|center]] | ||
− | | | + | | [[Place-Anywhere 7 Linear RCS Port{{if lang}}|{{Dict/part name|Place-Anywhere 7 Linear RCS Port}}]] |
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{{Radial Size/Cell|r}} | {{Radial Size/Cell|r}} | ||
| {{Formatnum/SortCell|25}} | | {{Formatnum/SortCell|25}} | ||
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| {{SortCell|3}}[[File:Vernor.png|60x60px|center]] | | {{SortCell|3}}[[File:Vernor.png|60x60px|center]] | ||
− | | {{if lang | + | | [[Vernor Engine{{if lang}}|{{Dict/part name|Vernor Engine}}]]<ref group="{{Dict|Note}}">{{lang |
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− | }}<ref group="{{Dict|Note}}">{{lang | ||
|en=The Vernor Engine uses a [[liquid fuel]]/[[oxidizer]] mixture. | |en=The Vernor Engine uses a [[liquid fuel]]/[[oxidizer]] mixture. | ||
+ | |fr=Le propulseur Vernor utilise un mélange [[Liquid fuel/fr|Ergol liquide]]/[[Oxidizer/fr|Oxydant]]. | ||
|de=Die Vernor Engine verwendetet die Flüßigtreibstoff/Oxidationsmittel-Mischung | |de=Die Vernor Engine verwendetet die Flüßigtreibstoff/Oxidationsmittel-Mischung | ||
|ru=Двигатель ориентации "Повулятор" использует смесь [[liquid fuel/ru|жидкого топлива]] и [[oxidizer/ru|окислителя]], аналогично обычным ракетным двигателям. | |ru=Двигатель ориентации "Повулятор" использует смесь [[liquid fuel/ru|жидкого топлива]] и [[oxidizer/ru|окислителя]], аналогично обычным ракетным двигателям. |
Revision as of 19:49, 8 June 2019
Image | Part | Radial size | Cost ( ![]() |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
Thrust (kN) |
Fuel ( ![]() |
Isp (s) (atm) | Isp (s) (vac) |
---|---|---|---|---|---|---|---|---|---|---|---|
RV-105 RCS Thruster Block | Radial mounted | 45 | 0.04 | 1 500 | 15 | 50 | 1.0 | 0.11 | 100 | 240 | |
Place-Anywhere 7 Linear RCS Port | Radial mounted | 25 | 0.02 | 2 600 | 15 | 50 | 2.0 | 0.21 | 100 | 240 | |
Vernor Engine[Note 1] | Radial mounted | 150 | 0.08 | 2 000 | 15 | 50 | 12.0 | 0.94 | 140 | 260 |
- ↑ The Vernor Engine uses a liquid fuel/oxidizer mixture.