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

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(Added Rocket part of R.A.P.I.E.R. in)
(Added "es" (spanish) translation)
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|pl=[[w:pl:Impuls_właściwy|I<sub>sp</sub>]] ([[w:pl:Sekunda|s]])
 
|pl=[[w:pl:Impuls_właściwy|I<sub>sp</sub>]] ([[w:pl:Sekunda|s]])
 
|ko=[[w:ko:비추력|비추력]] ([[w:ko:초 (시간)|초]])
 
|ko=[[w:ko:비추력|비추력]] ([[w:ko:초 (시간)|초]])
|de=[[w:de:Spezifischer_Impuls|ISP]] ([[w:de:Sekunde|s]])
+
|de=[[w:de:Spezifischer_Impuls|I<sub>sp</sub>]] ([[w:de:Sekunde|s]])
 +
|se=[[w:es:Impulso específico|I<sub>sp</sub>]]
 
}}
 
}}
 
!colspan=1|{{lang
 
!colspan=1|{{lang
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|ko=[[w:ko:추력편향|추력편향]]
 
|ko=[[w:ko:추력편향|추력편향]]
 
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
 
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
 +
|es=[[w:es:Empuje Vectorial|Empuje Vectorial]]
 
}}
 
}}
 
!colspan=3|{{lang
 
!colspan=3|{{lang
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|pl=Wlot
 
|pl=Wlot
 
|ko=흡입공기
 
|ko=흡입공기
|de=Lufteinlass}}
+
|de=Lufteinlass
 +
|es=Toma de aire
 +
}}
 
|-
 
|-
 
{{Stats Table Header|s|m|d|t|m}}
 
{{Stats Table Header|s|m|d|t|m}}
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|ko=추력 ([[w:ko:뉴턴 (단위)|kN]]
 
|ko=추력 ([[w:ko:뉴턴 (단위)|kN]]
 
|de=Schub ([[w:de:Newton_(Einheit)|kN]]
 
|de=Schub ([[w:de:Newton_(Einheit)|kN]]
 +
|es=Fuerza de empuje ([[w:es:Newton (física)|kN]]
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang
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|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]
 
|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]
 
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
 
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
 +
|es=[[w:es:Relación empuje a peso|Relación empuje a peso]]
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang
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|ko=[[w:ko:로켓 연료|연료]] ([[w:Flow_measurement|L/s]])
 
|ko=[[w:ko:로켓 연료|연료]] ([[w:Flow_measurement|L/s]])
 
|de=[[w:de:Raketentreibstoff|Raketenreibstoff]] ([[w:de:Massenstrom|L/s]])
 
|de=[[w:de:Raketentreibstoff|Raketenreibstoff]] ([[w:de:Massenstrom|L/s]])
 +
|en=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (l/s)
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang
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|ko=[[w:ko:기압|대기권]]
 
|ko=[[w:ko:기압|대기권]]
 
|de=[[w:de:Atmosphäre_(Astronomie)|atm]]
 
|de=[[w:de:Atmosphäre_(Astronomie)|atm]]
 +
|es=[[w:es:Atmósfera (unidad)|atm]]
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang
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|ko=[[w:ko:짐벌|짐벌]] ([[w:ko:도 (각도)|°]])
 
|ko=[[w:ko:짐벌|짐벌]] ([[w:ko:도 (각도)|°]])
 
|de=[[w:de:Schubvektorsteuerung|Schubvektorsteuerung]] ([[w:de:Grad_(Winkel)|°]])
 
|de=[[w:de:Schubvektorsteuerung|Schubvektorsteuerung]] ([[w:de:Grad_(Winkel)|°]])
 +
|es=[[w:es:Gimbal|Gimbal]] ([[w:es:Grado sexagesimal|º]])
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang
|en=Airflow|ru=воздушный поток
+
|en=Airflow
 +
|ru=воздушный поток
 
|pl=Przepływ Powietrza
 
|pl=Przepływ Powietrza
 
|ko=공기흐름
 
|ko=공기흐름
 
|de=Luftdurchlass
 
|de=Luftdurchlass
 +
|es=Flujo de aire
 
}}
 
}}
 
! scope="col" width="40px" | {{lang
 
! scope="col" width="40px" | {{lang
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|ko=크기
 
|ko=크기
 
|de=Größe
 
|de=Größe
 +
|es=Tamaño
 
}}
 
}}
 
! scope="col" width="40px" | {{lang
 
! scope="col" width="40px" | {{lang
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|ko=출력
 
|ko=출력
 
|de=Kraft
 
|de=Kraft
 +
|es=Potencia
 
}}
 
}}
  
 
|-
 
|-
 
| [[Image:Basic_jet_engine-t.png|60x60px|]]
 
| [[Image:Basic_jet_engine-t.png|60x60px|]]
| {{if lang link|Basic Jet Engine}}
+
| {{if lang link|Basic Jet Engine|es=Motor jet básico}}
 
| {{Radial Size|small}}
 
| {{Radial Size|small}}
 
| 950
 
| 950
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|-
 
|-
 
| [[Image:Rapier_Engine_01.png|60x60px|]]
 
| [[Image:Rapier_Engine_01.png|60x60px|]]
| {{if lang link|R.A.P.I.E.R. Engine}}
+
| {{if lang link|R.A.P.I.E.R. Engine|es=Motor R.A.P.I.E.R}}
 
| {{Radial Size|small}}
 
| {{Radial Size|small}}
 
| 5900
 
| 5900
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|-
 
|-
 
| [[Image:Turbojet-t.png|60x60px|]]
 
| [[Image:Turbojet-t.png|60x60px|]]
| {{if lang link|TurboJet Engine}}
+
| {{if lang link|TurboJet Engine|es=Motor turbojet}}
 
| {{Radial Size|small}}
 
| {{Radial Size|small}}
 
| 2250
 
| 2250

Revision as of 11:18, 5 January 2014

Isp (s) TVC Intake
Image Part Radial size Cost
(Funds)
Mass
(t)
Drag Max. Temp.
(K)
Tolerance
(m/s)
Thrust (kN) T/W ratio Combustible (l/s) atm Gimbal (°) Airflow Size Power
File:Basic jet engine-t.png Basic Jet Engine Small 950 1 0.2 3600 7 150 15.3 0.0955 1456 stall

7282 max

1.0 200 1.1 125
Rapier Engine 01.png R.A.P.I.E.R. Engine Small 5900 1.75 0.2 3600 20 225 10.2 0.30 800 stall

2524.332 max

3.0 - - -
File:Turbojet-t.png TurboJet Engine Small 2250 1.2 0.2 3600 7 225 19.1 0.358 546 stall

8192 max

1.0 60 1.0 200