Difference between revisions of "Template:Stats Table Jet Engines"
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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]]) | ||
| − | | | + | |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 ( | + | |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]]) | ||
| − | | | + | |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 (  ) |
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 |
|
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 |
