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

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{| class="wikitable sortable" style=white-space:nowrap
 
{| class="wikitable sortable" style=white-space:nowrap
 
|-
 
|-
{{Stats Table Header|s|m|d|t|m}}
+
{{Stats Table Header|r|m||t|m|t}}
! scope="col" width="60px" | {{lang
+
! scope="col" width="50px" | {{Dict/header|Thrust}}
|en=Thrust ([[w:Newton_(unit)|kN]])
+
! scope="col" width="50px" | {{Dict/header|TWR}}
|ru=Тяга ([[w:ru:Ньютон_(единица_измерения)|кН]])
+
! scope="col" width="50px" | {{lang
|pl=Ciąg ([[w:pl:Niuton|kN]])
+
|en=[[Liquid fuel|Fuel]]<br>({{Mark|fuelflow}})
|ko=추력 ([[w:ko:뉴턴 (단위)|kN]]
+
|fr=[[Liquid fuel/fr|Carburant]]<br>({{Mark|fuelflow}})
|de=Schub ([[w:de:Newton_(Einheit)|kN]]
+
|ru=[[w:ru:Ракетное_топливо|Расход<br>топлива]]<br>({{Mark|fuelflow}})
|es=Fuerza de empuje ([[w:es:Newton (unidad)|kN]])
+
|pl=[[Liquid fuel/pl|Paliwo]]<br>({{Mark|fuelflow}})
|hr=Potisak ([[w:hr:Njutn)|kN]])
+
|ko=[[w:ko:로켓 연료|연료]]<br>({{Mark|fuelflow}})
|hu=Tolóerő ([[w:hu:Newton_(mértékegység)|kN]])
+
|de=[[w:de:Raketentreibstoff|Raketenreibstoff]]<br>({{Mark|fuelflow}})
|ja=推力([[w:ja:ニュートン|kN]])
+
|es=[[w:es:Propelente#Propulsión de cohetes|Combustible]]<br>({{Mark|fuelflow}})
 +
|hr=Potrošnja goriva<br>({{Mark|fuelflow}})
 +
|hu=[[Liquid fuel/hu|Üzemanyag]]<br>({{Mark|fuelflow}})
 +
|ja=燃料[[w:ja:流量|流量]]<br>({{Mark|fuelflow}})
 
}}
 
}}
! scope="col" width="60px" | {{lang
+
! scope="col" width="50px" | {{lang
|en=[[Thrust-to-weight ratio|TWR]]
+
|en=[[Intake air|Intake]]<br>({{Mark|airu}}/{{Dict|s}})
|ru=[[w:ru:Тяговооружённость|Тяговооружённость]]
+
|fr=[[Intake air/fr|Entrée<br>d'air]]({{Mark|airu}}/{{Dict|s}})
|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]
+
|es=[[Intake air/es|Entrada de aire]]<br>({{Mark|airu}}/{{Dict|s}})
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
 
|es=[[w:es:Relación empuje a peso|Relación empuje a peso]]
 
|hr=Omjer potiska i težine
 
|hu=[[Thrust-to-weight ratio/hu|TWR]]
 
|ja=[[w:ja:推力重量比|推重比]]
 
 
}}
 
}}
! scope="col" width="60px" | {{lang
+
! scope="col" width="50px" | {{Dict/header|Isp}}
|en=[[Liquid fuel|Fuel]] ([[w:Flow_measurement|L/s]])
+
! scope="col" width="50px" | {{lang
|ru=[[w:ru:Ракетное_топливо|топливо]] ([[w:ru:Расходомер|L/s]])
+
|en=[[Thrust vectoring|TVC]]<br>([[w:Degree_(angle)|°]])
|pl=[[Liquid fuel/pl|Paliwo]] ([[w:pl:Przepływomierz|L/s]])
+
|fr=[[w:fr:Poussée vectorielle|Poussée<br>vectorielle]])
|ko=[[w:ko:로켓 연료|연료]] ([[w:Flow_measurement|L/s]])
+
|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]]<br>([[w:ru:Градус_(геометрия)|°]])
|de=[[w:de:Raketentreibstoff|Raketenreibstoff]] ([[w:de:Massenstrom|L/s]])
+
|pl=[[w:pl:Ciąg_wektorowany|TVC]]<br>([[w:pl:Stopień_(kąt)|°]])
|es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (l/s)
+
|ko=[[w:ko:추력편향|추력편향]]<br>([[w:ko:도 (각도)|°]])
|hr=Potrošnja goriva (L/s)
+
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]<br>([[w:de:Grad_(Winkel)|°]])
|hu=[[Liquid fuel/hu|Üzemanyag]] ({{mark|fuelu}}/s)
+
|es=[[w:es:Empuje vectorial|Empuje vectorial]]<br>([[w:es:Grado sexagesimal|º]])
|ja=燃料[[w:ja:流量|流量]](L/s)
+
|hr=[[w:hr:Vektorski potisak|Vektorski potisak]]<br>(°)
 +
|hu=[[w:hu:Tolóerővektor-eltérítés|TVC]]<br>([[w:hu:Fok (szög)|°]])
 +
|ja=[[w:ja:推力偏向|推力偏向]]<br>(°)
 
}}
 
}}
! scope="col" width="60px" | {{lang
+
! scope="col" width="50px" | {{lang
|en=[[Specific impulse|I<sub>sp</sub>]] ([[w:Second|s]])
+
|en=Reverse
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] ([[wikipedia:ru:Секунда|с]])
+
|fr=Inversion
|pl=[[w:pl:Impuls_właściwy|I<sub>sp</sub>]] ([[w:pl:Sekunda|s]])
+
|ru=Реверс
|ko=[[w:ko:비추력|비추력]] ([[w:ko:초 (시간)|초]])
+
|pl=Odwracać
|de=[[w:de:Spezifischer_Impuls|I<sub>sp</sub>]] ([[w:de:Sekunde|s]])
+
|ko=거꾸로 되다
|es=[[w:es:Impulso específico|I<sub>sp</sub>]] ([[w:es:Segundo|s]])
+
|de=Umkehren
|hr=[[w:hr:Specifični impuls|I<sub>sp</sub>]] ([[w:hr:Sekunda|s]])
+
|es=Dar marcha atrás
|hu=[[Specific impulse/hu|I<sub>sp</sub>]] ([[w:hu:Másodperc|s]])
+
|hr=Preokrenuti
|ja=[[w:ja:比推力|比推力]](秒)
+
|hu=Hátramenet
}}
+
|ja=リバース
! scope="col" width="60px" | {{lang
 
|en=[[Thrust vectoring|TVC]] ([[w:Degree_(angle)|°]])
 
|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]] ([[w:ru:Градус_(геометрия)|°]])
 
|pl=[[w:pl:Ciąg_wektorowany|TVC]] ([[w:pl:Stopień_(kąt)|°]])
 
|ko=[[w:ko:추력편향|추력편향]] ([[w:ko:도 (각도)|°]])
 
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]] ([[w:de:Grad_(Winkel)|°]])
 
|es=[[w:es:Empuje vectorial|Empuje vectorial]] ([[w:es:Grado sexagesimal|º]])
 
|hr=[[w:hr:Vektorski potisak|Vektorski potisak]]
 
|hu=[[w:hu:Tolóerővektor-eltérítés|TVC]] ([[w:hu:Fok_(szög)|°]])
 
|ja=[[w:ja:推力偏向|推力偏向]](°)
 
 
}}
 
}}
 
|-
 
|-
| [[File:Turbojetengine.png|60x60px|center]]
+
| {{SortCell|1}}[[File:J90JunoBasicJetEngine.png|60x60px|center]]
| {{if lang link|TurboJet Engine
+
| [[J-20 "Juno" Basic Jet Engine{{if lang}}|{{Dict/part name|J-20 "Juno" Basic Jet Engine}}]]
|es=Motor turbojet
+
{{Radial Size/Cell|0}}
|hr=Turbomlazni motor
+
| {{Formatnum/SortCell|450}}
|hu=Turbojet Hajtómű
+
| {{Formatnum/SortCell|0.25|2}}
|ru=Турбо-реактивный двигатель}}
+
| {{Formatnum/SortCell|2000}}
| {{Radial Size|small}}
+
| 7
 +
| 50
 +
| {{Formatnum/SortCell|20|1}} <sub>Mach 0</sub><br>{{Formatnum|20.6|1}} <sub>Mach {{Formatnum|1.3|1}}</sub>
 +
| {{Formatnum/SortCell|8.16|2}} <sub>Mach 0</sub><br>{{Formatnum|8.40|2}} <sub>Mach {{Formatnum|1.3|1}}</sub>
 +
| {{Formatnum/SortCell|0.064|3}}
 +
| {{Formatnum/SortCell|1.402|3}}
 +
| {{Formatnum/SortCell|6400}}
 +
| {{SortCell|0}}—
 +
| {{No}}
 +
|-
 +
| {{SortCell|2}}[[File:J33WheesleyBasicJetEngine.png|60x60px|center]]
 +
| [[J-33 "Wheesley" Turbofan Engine{{if lang}}|{{Dict/part name|J-33 "Wheesley" Turbofan Engine}}]]
 +
{{Radial Size/Cell|1}}
 +
| {{Formatnum/SortCell|1400}}
 +
| {{Formatnum/SortCell|1.5|1}}
 +
| {{Formatnum/SortCell|2000}}
 +
| 7
 +
| 50
 +
| {{Formatnum/SortCell|120|1}} <sub>Mach 0</sub>
 +
| {{Formatnum/SortCell|8.16|2}} <sub>Mach 0</sub>
 +
| {{Formatnum/SortCell|0.233|3}}
 +
| {{Formatnum/SortCell|29.601|3}}
 +
| {{Formatnum/SortCell|10500}}
 +
| {{SortCell|0}}—
 +
| {{Yes}}
 +
|-
 +
| {{SortCell|3}}[[File:J404PantherAfterburningTurbofan.png|60x60px|center]]
 +
| [[J-404 "Panther" Afterburning Turbofan{{if lang}}|{{Dict/part name|J-404 "Panther" Afterburning Turbofan}}]]
 +
{{Radial Size/Cell|1}}
 +
| {{Formatnum/SortCell|2000}}
 +
| {{Formatnum/SortCell|1.2|1}}
 +
| {{Formatnum/SortCell|2000}}
 +
| 7
 +
| 50
 +
| {{Formatnum/SortCell|85|2}} <sub>Mach 0</sub><br>{{Formatnum|107.89|2}} <sub>Mach {{Formatnum|1.75|2}}</sub> /<br>{{Formatnum|130|2}} <sub>Mach 0</sub><br>{{Formatnum|219.48|2}} <sub>Mach {{Formatnum|2.5|1}}</sub>
 +
| {{Formatnum/SortCell|7.22|2}} <sub>Mach 0</sub><br>{{Formatnum|9.17|2}} <sub>Mach {{Formatnum|1.75|2}}</sub> /<br>{{Formatnum|11.05|2}} <sub>Mach 0</sub><br>{{Formatnum|18.65|2}} <sub>Mach {{Formatnum|2.5|1}}</sub>
 +
| {{Formatnum/SortCell|0.193|3}} /<br>{{Formatnum|0.663|3}}
 +
| {{Formatnum/SortCell|7.705|3}} /<br>{{Formatnum|7.954|3}}
 +
| {{Formatnum/SortCell|9000}} /<br>{{Formatnum|4000}}
 +
| {{Formatnum/SortCell|10|1}}
 +
| {{No}}
 +
|-
 +
| {{SortCell|4}}[[File:JX4WhiplashTurboRamjetEngine.png|60x60px|center]]
 +
| [[J-X4 "Whiplash" Turbo Ramjet Engine{{if lang}}|{{Dict/part name|J-X4 "Whiplash" Turbo Ramjet Engine}}]]
 +
{{Radial Size/Cell|1}}
 
| {{Formatnum/SortCell|2250}}
 
| {{Formatnum/SortCell|2250}}
| {{Formatnum/SortCell|1.2|1}}
+
| {{Formatnum/SortCell|1.8|1}}
| {{Formatnum/SortCell|0.2|1}}
+
| {{Formatnum/SortCell|2000}}
| {{Formatnum/SortCell|3600}}
 
 
| 7
 
| 7
| 225
+
| 50
| {{Formatnum/SortCell|19.1|1}}
+
| {{Formatnum/SortCell|130|2}} <sub>Mach 0</sub><br>{{Formatnum|386.66|2}} <sub>Mach {{Formatnum|3|1}}</sub>
| {{Formatnum/SortCell|0.358|3}}
+
| {{Formatnum/SortCell|7.36|2}} <sub>Mach 0</sub><br>{{Formatnum|21.9|2}} <sub>Mach {{Formatnum|3|1}}</sub>
| {{Formatnum/SortCell|8192}} <sub>max</sub>
+
| {{Formatnum/SortCell|0.663|3}}
546 <sub>stall</sub>
+
| {{Formatnum/SortCell|5.303|3}}
 +
| {{Formatnum/SortCell|4000}}
 
| {{Formatnum/SortCell|1|1}}
 
| {{Formatnum/SortCell|1|1}}
 +
| {{No}}
 
|-
 
|-
| [[File:Basicjetengine.png|60x60px|center]]
+
| {{SortCell|5}}[[File:J-90 Goliath Turbofan Engine.png|60x60px|center]]
| {{if lang link|Basic Jet Engine
+
| [[J-90 "Goliath" Turbofan Engine{{if lang}}|{{Dict/part name|J-90 "Goliath" Turbofan Engine}}]]
|es=Motor jet básico
+
{{Radial Size/Cell|r}}
|hr=Osnovni mlazni motor
+
| {{Formatnum/SortCell|2600}}
|hu=Basic Sugárhajtómű
+
| {{Formatnum/SortCell|4.5|1}}
|ru=Основной воздушно-реактивный двигатель}}
+
| {{Formatnum/SortCell|2000}}
| {{Radial Size|small}}
 
| 950
 
| 1
 
| {{Formatnum/SortCell|0.2|1}}
 
| {{Formatnum/SortCell|3600}}
 
 
| 7
 
| 7
| 150
+
| 50
| {{Formatnum/SortCell|15.3|1}}
+
| {{Formatnum/SortCell|360|1}} <sub>Mach 0</sub>
| {{Formatnum/SortCell|0.0955|4}}
+
| {{Formatnum/SortCell|8.16|2}} <sub>Mach 0</sub>
| {{Formatnum/SortCell|7282}} <sub>max</sub>
+
| {{Formatnum/SortCell|0.583|3}}
1456 <sub>stall</sub>
+
| {{Formatnum/SortCell|132.273|3}}
| {{Formatnum/SortCell|1|1}}
+
| {{Formatnum/SortCell|12600}}
 +
| {{SortCell|0}}—
 +
| {{Yes}}
 
|-
 
|-
| [[File:Rapier_Engine_01.png|60x60px|center]]
+
| {{SortCell|6}}[[File:Rapier_Engine_01.png|60x60px|center]]
| {{if lang link|R.A.P.I.E.R. Engine
+
| [[CR-7 R.A.P.I.E.R. Engine{{if lang}}|{{Dict/part name|CR-7 R.A.P.I.E.R. Engine}}]]<ref group="{{Dict|Note}}">{{lang
|es=Motor R.A.P.I.E.R.
 
|hr=Motor R.A.P.I.E.R.
 
|hu=R.A.P.I.E.R. Hajtómű
 
|ru=Двигатель "R.A.P.I.E.R."
 
}}<ref group="{{dict|Note}}">{{lang
 
 
|en=The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the jet engine properties are shown.
 
|en=The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the jet engine properties are shown.
 +
|fr=Le propulseur R.A.P.I.E.R. est une combinaison de propulseur à ergol liquid et de moteur à réaction. Seules les propriétés en mode moteur à réaction sont affichées.
 
|de=Die R.A.P.I.E.R. Engine ist eine Kombination eines Raketentriebwerks und Jettriebwerks. Nur die Eigenschaften des Jettriebwerks werden aufgelistet.
 
|de=Die R.A.P.I.E.R. Engine ist eine Kombination eines Raketentriebwerks und Jettriebwerks. Nur die Eigenschaften des Jettriebwerks werden aufgelistet.
 
|hu=A R.A.P.I.E.R. egy sugár-rakéta kettős üzemmódra tervezett speciális hajtómű. Itt csak a sugárhajtómű üzemmód alatti tulajdonságai látszódnak
 
|hu=A R.A.P.I.E.R. egy sugár-rakéta kettős üzemmódra tervezett speciális hajtómű. Itt csak a sugárhajtómű üzemmód alatti tulajdonságai látszódnak
|ru=Двигатель "R.A.P.I.E.R." сочетает в себе воздушно-реактивный и ракетный двигатели. Показаны свойства только воздушно-реактивного двигателя.
+
|ru=Двигатель R.A.P.I.E.R. является комбинацией [[w:ru:Жидкостный_ракетный_двигатель|ЖРД]] и [[w:ru:Воздушно-реактивный_двигатель|ВРД]]. Показаны только параметры, относящиеся к ВРД.
 
|ja=R.A.P.I.E.R.エンジンは液体燃料エンジンとしてもジェットエンジンとしても機能するため、本項ではジェットエンジンとしての性能のみを記載する。
 
|ja=R.A.P.I.E.R.エンジンは液体燃料エンジンとしてもジェットエンジンとしても機能するため、本項ではジェットエンジンとしての性能のみを記載する。
 +
|ko=R.A.P.I.E.R 엔진은 액체연료 엔진 모드와 제트 엔진 모드로 사용할 수 있습니다. 여기서는 제트 엔진으로써의 성능만을 기재합니다
 +
|es=El R.A.P.I.E.R. El motor es una combinación de combustible líquido y motor a reacción. Sólo se muestran las propiedades del motor a reacción.
 
}}</ref>
 
}}</ref>
| {{Radial Size|small}}
+
{{Radial Size/Cell|1}}
| {{Formatnum/SortCell|3600}}
+
| {{Formatnum/SortCell|6000}}
| {{Formatnum/SortCell|1.2|1}}
+
| {{Formatnum/SortCell|2|1}}
| {{Formatnum/SortCell|0.2|1}}
+
| {{Formatnum/SortCell|2000}}
| {{Formatnum/SortCell|3600}}
 
 
| 20
 
| 20
| 190
+
| 50
| {{Formatnum/SortCell|16.1|1}}
+
| {{Formatnum/SortCell|105|2}} <sub>Mach 0</sub><br>{{Formatnum|465.64|2}} <sub>Mach {{Formatnum|3.75|2}}</sub>
| {{Formatnum/SortCell|0.3|2}}
+
| {{Formatnum/SortCell|5.35|2}} <sub>Mach 0</sub><br>{{Formatnum|23.74|2}} <sub>Mach {{Formatnum|3.75|2}}</sub>
| {{Formatnum/SortCell|2524.332}} <sub>max</sub>  
+
| {{Formatnum/SortCell|0.669|3}}
800 <sub>stall</sub>
+
| {{Formatnum/SortCell|4.015|3}}
 +
| {{Formatnum/SortCell|3200}}
 
| {{Formatnum/SortCell|3|1}}
 
| {{Formatnum/SortCell|3|1}}
|-
+
| {{No}}
 
|}
 
|}
<small><references group="{{dict|Note}}" /></small>
+
<small><references group="{{Dict|Note}}" /></small>
 +
 
 +
<!--v1.7-->
 +
<noinclude>[[Category:Template:Stats Tables]]</noinclude>

Latest revision as of 09:56, 11 June 2019

Image Part Radial size Cost
(Funds)
Mass
(t)
Max. Temp.
(K)
Tolerance
(m/s)
Tolerance
(g)
Thrust
(kN)
TWR Fuel
(Units of fuel/s)
Intake
(Air unit/s)
Isp (s) TVC
(°)
Reverse
J90JunoBasicJetEngine.png
J-20 "Juno" Basic Jet Engine Tiny 450 0.25 2 000 7 50 20.0 Mach 0
20.6 Mach 1.3
8.16 Mach 0
8.40 Mach 1.3
0.064 1.402 6 400 No
J33WheesleyBasicJetEngine.png
J-33 "Wheesley" Turbofan Engine Small 1 400 1.5 2 000 7 50 120.0 Mach 0 8.16 Mach 0 0.233 29.601 10 500 Yes
J404PantherAfterburningTurbofan.png
J-404 "Panther" Afterburning Turbofan Small 2 000 1.2 2 000 7 50 85.00 Mach 0
107.89 Mach 1.75 /
130.00 Mach 0
219.48 Mach 2.5
7.22 Mach 0
9.17 Mach 1.75 /
11.05 Mach 0
18.65 Mach 2.5
0.193 /
0.663
7.705 /
7.954
9 000 /
4 000
10.0 No
JX4WhiplashTurboRamjetEngine.png
J-X4 "Whiplash" Turbo Ramjet Engine Small 2 250 1.8 2 000 7 50 130.00 Mach 0
386.66 Mach 3.0
7.36 Mach 0
21.90 Mach 3.0
0.663 5.303 4 000 1.0 No
J-90 Goliath Turbofan Engine.png
J-90 "Goliath" Turbofan Engine Radial mounted 2 600 4.5 2 000 7 50 360.0 Mach 0 8.16 Mach 0 0.583 132.273 12 600 Yes
Rapier Engine 01.png
CR-7 R.A.P.I.E.R. Engine[Note 1] Small 6 000 2.0 2 000 20 50 105.00 Mach 0
465.64 Mach 3.75
5.35 Mach 0
23.74 Mach 3.75
0.669 4.015 3 200 3.0 No
  1. The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the jet engine properties are shown.