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
 
|-
 
|-
−
!colspan=11|
+
{{Stats Table Header|r|m||t|m|t}}
−
!colspan=1|{{lang
+
! scope="col" width="50px" | {{Dict/header|Thrust}}
−
|en=[[w:Specific_impulse|I<sub>sp</sub>]] ([[w:Second|s]])
+
! scope="col" width="50px" | {{Dict/header|TWR}}
−
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] ([[wikipedia:ru:Секунда|с]])
+
! scope="col" width="50px" | {{lang
−
|pl=[[w:pl:Impuls_właściwy|I<sub>sp</sub>]] ([[w:pl:Sekunda|s]])
+
|en=[[Liquid fuel|Fuel]]<br>({{Mark|fuelflow}})
−
|ko=[[w:ko:비추력|비추력]] ([[w:ko:초 (시간)|초]])
+
|fr=[[Liquid fuel/fr|Carburant]]<br>({{Mark|fuelflow}})
−
|de=[[w:de:Spezifischer_Impuls|I<sub>sp</sub>]] ([[w:de:Sekunde|s]])
+
|ru=[[w:ru:Ракетное_топливо|Расход<br>топлива]]<br>({{Mark|fuelflow}})
−
|es=[[w:es:Impulso específico|I<sub>sp</sub>]] ([[w:es:Segundo|s]])
+
|pl=[[Liquid fuel/pl|Paliwo]]<br>({{Mark|fuelflow}})
−
|hr=[[w:hr:Specifični impuls|I<sub>sp</sub>]] ([[w:hr:Sekunda|s]])
+
|ko=[[w:ko:로켓 연료|연료]]<br>({{Mark|fuelflow}})
 +
|de=[[w:de:Raketentreibstoff|Raketenreibstoff]]<br>({{Mark|fuelflow}})
 +
|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}})
 
}}
 
}}
−
!colspan=1|{{lang
+
! scope="col" width="50px" | {{lang
−
|en=[[w:Thrust_Vectoring|TVC]]
+
|en=[[Intake air|Intake]]<br>({{Mark|airu}}/{{Dict|s}})
−
|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]]
+
|fr=[[Intake air/fr|Entrée<br>d'air]]({{Mark|airu}}/{{Dict|s}})
−
|pl=[[w:pl:Ciąg_wektorowany|TVC]]
+
|es=[[Intake air/es|Entrada de aire]]<br>({{Mark|airu}}/{{Dict|s}})
−
|ko=[[w:ko:추력편향|추력편향]]
 
−
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
 
−
|es=[[w:es:Empuje vectorial|Empuje vectorial]]
 
−
|hr=[[w:hr:Vektorski potisak|Vektorski potisak]]
 
 
}}
 
}}
−
!colspan=3|{{lang
+
! scope="col" width="50px" | {{Dict/header|Isp}}
−
|en=Intake
+
! scope="col" width="50px" | {{lang
−
|ru=впускного
+
|en=[[Thrust vectoring|TVC]]<br>([[w:Degree_(angle)|°]])
−
|pl=Wlot
+
|fr=[[w:fr:Poussée vectorielle|Poussée<br>vectorielle]](°)
−
|ko=흡입공기
+
|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]]<br>([[w:ru:Градус_(геометрия)|°]])
−
|de=Lufteinlass
+
|pl=[[w:pl:Ciąg_wektorowany|TVC]]<br>([[w:pl:Stopień_(kąt)|°]])
−
|es=Toma de aire
+
|ko=[[w:ko:추력편향|추력편향]]<br>([[w:ko:도 (각도)|°]])
−
|hr=Usis
+
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]<br>([[w:de:Grad_(Winkel)|°]])
 +
|es=[[w:es:Empuje vectorial|Empuje vectorial]]<br>([[w:es:Grado sexagesimal|º]])
 +
|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="50px" | {{lang
 +
|en=Reverse
 +
|fr=Inversion
 +
|ru=Реверс
 +
|pl=Odwracać
 +
|ko=거꾸로 되다
 +
|de=Umkehren
 +
|es=Dar marcha atrás
 +
|hr=Preokrenuti
 +
|hu=Hátramenet
 +
|ja=リバース
 +
}}
 +
|-
 +
| {{SortCell|1}}[[File:J90JunoBasicJetEngine.png|60x60px|center]]
 +
| [[J-20 "Juno" Basic Jet Engine{{if lang}}|{{Dict/part name|J-20 "Juno" Basic Jet Engine}}]]
 +
{{Radial Size/Cell|0}}
 +
| {{Formatnum/SortCell|450}}
 +
| {{Formatnum/SortCell|0.25|2}}
 +
| {{Formatnum/SortCell|2000}}
 +
| 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}}
 
|-
 
|-
−
{{Stats Table Header|s|m|d|t|m}}
+
| {{SortCell|3}}[[File:J404PantherAfterburningTurbofan.png|60x60px|center]]
−
! scope="col" width="60px" | {{lang
+
| [[J-404 "Panther" Afterburning Turbofan{{if lang}}|{{Dict/part name|J-404 "Panther" Afterburning Turbofan}}]]
−
|en=Thrust ([[w:Newton_(unit)|kN]])
+
{{Radial Size/Cell|1}}
−
|ru=Тяга ([[w:ru:Ньютон_(единица_измерения)|кН]])
+
| {{Formatnum/SortCell|2000}}
−
|pl=Ciąg ([[w:pl:Niuton|kN]])
+
| {{Formatnum/SortCell|1.2|1}}
−
|ko=추력 ([[w:ko:뉴턴 (단위)|kN]]
+
| {{Formatnum/SortCell|2000}}
−
|de=Schub ([[w:de:Newton_(Einheit)|kN]]
+
| 7
−
|es=Fuerza de empuje ([[w:es:Newton (unidad)|kN]])
+
| 50
−
|hr=Potisak ([[w:hr:Njutn)|kN]])
+
| {{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>
−
! scope="col" width="60px" | {{lang
+
| {{Formatnum/SortCell|0.193|3}} /<br>{{Formatnum|0.663|3}}
−
|en=[[w:Thrust-to-weight_ratio|T/W ratio]]
+
| {{Formatnum/SortCell|7.705|3}} /<br>{{Formatnum|7.954|3}}
−
|ru=[[w:ru:Тяговооружённость|Тяговооружённость]]
+
| {{Formatnum/SortCell|9000}} /<br>{{Formatnum|4000}}
−
|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]
+
| {{Formatnum/SortCell|10|1}}
−
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
+
| {{No}}
−
|es=[[w:es:Relación empuje a peso|Relación empuje a peso]]
 
−
|hr=Omjer potiska i težine
 
−
}}
 
−
! scope="col" width="60px" | {{lang
 
−
|en=[[w:Rocket_propellant|Fuel]] ([[w:Flow_measurement|L/s]])
 
−
|ru=[[w:ru:Ракетное_топливо|топливо]] ([[w:ru:Расходомер|L/s]])
 
−
|pl=[[w:pl:Paliwo_rakietowe|Paliwo]]  ([[w:pl:Przepływomierz|L/s]])
 
−
|ko=[[w:ko:로켓 연료|연료]] ([[w:Flow_measurement|L/s]])
 
−
|de=[[w:de:Raketentreibstoff|Raketenreibstoff]] ([[w:de:Massenstrom|L/s]])
 
−
|es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (l/s)
 
−
|hr=Potrošnja goriva (L/s)
 
−
}}
 
−
! scope="col" width="60px" | {{lang
 
−
|en=[[w:Atmosphere_(unit)|atm]]
 
−
|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]
 
−
|pl=[[w:pl:Atmosfera_fizyczna|atm]]
 
−
|ko=[[w:ko:기압|대기권]]
 
−
|de=[[w:de:Atmosphäre_(Astronomie)|atm]]
 
−
|es=[[w:es:Atmósfera (unidad)|atm]]
 
−
|hr=[[w:hr:Atmosfera|atm.]]
 
−
}}
 
−
! scope="col" width="60px" | {{lang
 
−
|en=[[w:Gimbal|Gimbal]] ([[w:Degree_(angle)|°]])
 
−
|ru=[[w:ru:Карданов_подвес|Карданов подвес]] ([[w:ru:Градус_(геометрия)|°]])
 
−
|pl=[[w:Gimbal|Gimbal]] ([[w:pl:Stopień_(kąt)|°]])
 
−
|ko=[[w:ko:짐벌|짐벌]] ([[w:ko:도 (각도)|°]])
 
−
|de=[[w:de:Schubvektorsteuerung|Schubvektorsteuerung]] ([[w:de:Grad_(Winkel)|°]])
 
−
|es=[[w:es:Gimbal|Gimbal]] ([[w:es:Grado sexagesimal|º]])
 
−
|hr=Kardanski ovjes
 
−
}}
 
−
! scope="col" width="60px" | {{lang
 
−
|en=Airflow
 
−
|ru=воздушный поток
 
−
|pl=Przepływ Powietrza
 
−
|ko=공기흐름
 
−
|de=Luftdurchlass
 
−
|es=Flujo de aire
 
−
|hr=Protok zraka
 
−
}}
 
−
! scope="col" width="40px" | {{lang
 
−
|en=Size
 
−
|ru=Размер
 
−
|pl=Rozmiar
 
−
|ko=크기
 
−
|de=Größe
 
−
|es=Tamaño
 
−
|hr=Veličina
 
−
}}
 
−
! scope="col" width="40px" | {{lang
 
−
|en=Power
 
−
|ru=Впускной
 
−
|pl=Moc
 
−
|ko=출력
 
−
|de=Kraft
 
−
|es=Potencia
 
−
|hr=Snaga
 
−
}}
 
 
|-
 
|-
−
| [[Image:Turbojet-t.png|60x60px|]]
+
| {{SortCell|4}}[[File:JX4WhiplashTurboRamjetEngine.png|60x60px|center]]
−
| {{if lang link|TurboJet Engine|es=Motor turbojet|hr=Turbomlazni motor}}
+
| [[J-X4 "Whiplash" Turbo Ramjet Engine{{if lang}}|{{Dict/part name|J-X4 "Whiplash" Turbo Ramjet Engine}}]]
−
| {{Radial Size|small}}
+
{{Radial Size/Cell|1}}
−
| 2250
+
| {{Formatnum/SortCell|2250}}
−
| 1.2
+
| {{Formatnum/SortCell|1.8|1}}
−
| 0.2
+
| {{Formatnum/SortCell|2000}}
−
| 3600
 
 
| 7
 
| 7
−
| 225
+
| 50
−
| 19.1
+
| {{Formatnum/SortCell|130|2}} <sub>Mach 0</sub><br>{{Formatnum|386.66|2}} <sub>Mach {{Formatnum|3|1}}</sub>
−
| 0.358
+
| {{Formatnum/SortCell|7.36|2}} <sub>Mach 0</sub><br>{{Formatnum|21.9|2}} <sub>Mach {{Formatnum|3|1}}</sub>
−
| 546 <sub>stall</sub>  
+
| {{Formatnum/SortCell|0.663|3}}
−
8192 <sub>max</sub>  
+
| {{Formatnum/SortCell|5.303|3}}
−
| 1.0
+
| {{Formatnum/SortCell|4000}}
−
| 60
+
| {{Formatnum/SortCell|1|1}}
−
| 1.0
+
| {{No}}
−
| 200
 
 
|-
 
|-
−
| [[Image:Basic_jet_engine-t.png|60x60px|]]
+
| {{SortCell|5}}[[File:J-90 Goliath Turbofan Engine.png|60x60px|center]]
−
| {{if lang link|Basic Jet Engine|es=Motor jet básico|hr=Osnovni mlazni motor}}
+
| [[J-90 "Goliath" Turbofan Engine{{if lang}}|{{Dict/part name|J-90 "Goliath" Turbofan Engine}}]]
−
| {{Radial Size|small}}
+
{{Radial Size/Cell|r}}
−
| 950
+
| {{Formatnum/SortCell|2600}}
−
| 1
+
| {{Formatnum/SortCell|4.5|1}}
−
| 0.2
+
| {{Formatnum/SortCell|2000}}
−
| 3600
 
 
| 7
 
| 7
−
| 150
+
| 50
−
| 15.3
+
| {{Formatnum/SortCell|360|1}} <sub>Mach 0</sub>
−
| 0.0955
+
| {{Formatnum/SortCell|8.16|2}} <sub>Mach 0</sub>
−
| 1456 <sub>stall</sub>
+
| {{Formatnum/SortCell|0.583|3}}
−
7282 <sub>max</sub>
+
| {{Formatnum/SortCell|132.273|3}}
−
| 1.0
+
| {{Formatnum/SortCell|12600}}
−
| 200
+
| {{SortCell|0}}—
−
| 1.1
+
| {{Yes}}
−
| 125
 
 
|-
 
|-
−
| [[Image:Rapier_Engine_01.png|60x60px|]]
+
| {{SortCell|6}}[[File:Rapier_Engine_01.png|60x60px|center]]
−
| {{if lang link|R.A.P.I.E.R. Engine|es=Motor R.A.P.I.E.R|hr=Motor R.A.P.I.E.R.}}<ref group="Note">The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the jet engine properties are shown.</ref>
+
| [[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
−
| {{Radial Size|small}}
+
|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.
−
| 5900
+
|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.
−
| 1.75
+
|de=Die R.A.P.I.E.R. Engine ist eine Kombination eines Raketentriebwerks und Jettriebwerks. Nur die Eigenschaften des Jettriebwerks werden aufgelistet.
−
| 0.2
+
|hu=A R.A.P.I.E.R. egy sugár-rakéta kettős üzemmódra tervezett speciális hajtómű. Itt csak a sugárhajtómű üzemmód alatti tulajdonságai látszódnak
−
| 3600
+
|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。
 +
|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>
 +
{{Radial Size/Cell|1}}
 +
| {{Formatnum/SortCell|6000}}
 +
| {{Formatnum/SortCell|2|1}}
 +
| {{Formatnum/SortCell|2000}}
 
| 20
 
| 20
−
| 225
+
| 50
−
| 10.2
+
| {{Formatnum/SortCell|105|2}} <sub>Mach 0</sub><br>{{Formatnum|465.64|2}} <sub>Mach {{Formatnum|3.75|2}}</sub>
−
| 0.30
+
| {{Formatnum/SortCell|5.35|2}} <sub>Mach 0</sub><br>{{Formatnum|23.74|2}} <sub>Mach {{Formatnum|3.75|2}}</sub>
−
| 800 <sub>stall</sub>  
+
| {{Formatnum/SortCell|0.669|3}}
−
2524.332 <sub>max</sub>  
+
| {{Formatnum/SortCell|4.015|3}}
−
| 3.0
+
| {{Formatnum/SortCell|3200}}
−
| -
+
| {{Formatnum/SortCell|3|1}}
−
| -
+
| {{No}}
−
| -
 
−
|-
 
 
|}
 
|}
−
<small><references group="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.
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