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

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(Added "es" (spanish) translation)
m
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|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|I<sub>sp</sub>]] ([[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>]]
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|es=[[w:es:Impulso específico|I<sub>sp</sub>]]
 
}}
 
}}
 
!colspan=1|{{lang
 
!colspan=1|{{lang
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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]]
+
|es=Fuerza de empuje ([[w:es:Newton (unidad)|kN]]
 
}}
 
}}
 
! 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)
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|es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (l/s)
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang

Revision as of 11:21, 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 Fuel (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