Difference between revisions of "Template:Stats Table Liquid Fuel Engines"
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(Added Cost, Drag, Max Temp, Tolerance, Thrust Vectoring & Gimbal Range. Defined column width for better compatibility with various monitor aspect ratios and general neatness.) |
m (Space saving. Combined Thrust Vectoring and Gimbal Range columns.) |
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| Line 7: | Line 7: | ||
|#default=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]] | |#default=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]] | ||
}} | }} | ||
| + | |||
!colspan=2|{{#switch:{{{1}}} | !colspan=2|{{#switch:{{{1}}} | ||
|=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | |=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]] | |ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]] | ||
|#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | |#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
| + | }} | ||
| + | |||
| + | !colspan=1|{{#switch:{{{1}}} | ||
| + | |=[[w:Thrust_Vectoring|TVC]] | ||
| + | |ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]] | ||
| + | |#default=[[w:Thrust_Vectoring|TVC]] | ||
}} | }} | ||
|- | |- | ||
| Line 18: | Line 25: | ||
|#default=Image | |#default=Image | ||
}} | }} | ||
| + | |||
! scope="col" width="256px" | {{#switch:{{{1}}} | ! scope="col" width="256px" | {{#switch:{{{1}}} | ||
|=Part | |=Part | ||
| Line 23: | Line 31: | ||
|#default=Part | |#default=Part | ||
}} | }} | ||
| + | |||
! scope="col" width="80px" | {{#switch:{{{1}}} | ! scope="col" width="80px" | {{#switch:{{{1}}} | ||
|=Size | |=Size | ||
| Line 28: | Line 37: | ||
|#default=Size | |#default=Size | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=Cost ($) | |=Cost ($) | ||
| Line 33: | Line 43: | ||
|#default=Cost ($) | |#default=Cost ($) | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | |=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
| Line 38: | Line 49: | ||
|#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | |#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Drag_(physics)|Drag]] | |=[[w:Drag_(physics)|Drag]] | ||
| Line 43: | Line 55: | ||
|#default=[[w:Drag_(physics)|Drag]] | |#default=[[w:Drag_(physics)|Drag]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=Max Temp [[w:Kelvin|(K)]] | |=Max Temp [[w:Kelvin|(K)]] | ||
| Line 48: | Line 61: | ||
|#default=Max Temp [[w:Kelvin|(K)]] | |#default=Max Temp [[w:Kelvin|(K)]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=Tolerance | |=Tolerance | ||
| Line 53: | Line 67: | ||
|#default=Tolerance | |#default=Tolerance | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=Thrust [[w:Newton_(unit)|(kN)]] | |=Thrust [[w:Newton_(unit)|(kN)]] | ||
| Line 58: | Line 73: | ||
|#default=Thrust [[w:Newton_(unit)|(kN)]] | |#default=Thrust [[w:Newton_(unit)|(kN)]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Thrust-to-weight_ratio|T/W ratio]] | |=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
| Line 63: | Line 79: | ||
|#default=[[w:Thrust-to-weight_ratio|T/W ratio]] | |#default=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Atmosphere_(unit)|atm]] | |=[[w:Atmosphere_(unit)|atm]] | ||
| Line 68: | Line 85: | ||
|#default=[[w:Atmosphere_(unit)|atm]] | |#default=[[w:Atmosphere_(unit)|atm]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Vacuum|vac]] | |=[[w:Vacuum|vac]] | ||
| Line 73: | Line 91: | ||
|#default=[[w:Vacuum|vac]] | |#default=[[w:Vacuum|vac]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Atmosphere_(unit)|atm]] | |=[[w:Atmosphere_(unit)|atm]] | ||
| Line 78: | Line 97: | ||
|#default=[[w:Atmosphere_(unit)|atm]] | |#default=[[w:Atmosphere_(unit)|atm]] | ||
}} | }} | ||
| + | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Vacuum|vac]] | |=[[w:Vacuum|vac]] | ||
| Line 83: | Line 103: | ||
|#default=[[w:Vacuum|vac]] | |#default=[[w:Vacuum|vac]] | ||
}} | }} | ||
| − | + | ||
| − | |||
| − | |||
| − | |||
| − | |||
! scope="col" width="60px" | {{#switch:{{{1}}} | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
|=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]] | |=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]] | ||
| Line 113: | Line 129: | ||
| 280 | | 280 | ||
| 330 | | 330 | ||
| − | |||
| 1.0 | | 1.0 | ||
|- | |- | ||
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| 320 | | 320 | ||
| 370 | | 370 | ||
| − | |||
| - | | - | ||
|- | |- | ||
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| 320 | | 320 | ||
| 370 | | 370 | ||
| − | |||
| 1.0 | | 1.0 | ||
|- | |- | ||
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| 300 | | 300 | ||
| 390 | | 390 | ||
| − | |||
| 0.5 | | 0.5 | ||
|- | |- | ||
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| 390 | | 390 | ||
| 390 | | 390 | ||
| − | |||
| - | | - | ||
|- | |- | ||
| Line 218: | Line 229: | ||
| 270 | | 270 | ||
| 390 | | 390 | ||
| − | |||
| 2.5 | | 2.5 | ||
|- | |- | ||
| Line 239: | Line 249: | ||
| 280 | | 280 | ||
| 330 | | 330 | ||
| − | |||
| 1.0 | | 1.0 | ||
|- | |- | ||
| Line 260: | Line 269: | ||
| 220 | | 220 | ||
| 800 | | 800 | ||
| − | |||
| 1.0 | | 1.0 | ||
|- | |- | ||
|} | |} | ||
Revision as of 22:19, 27 October 2012
| Fuel (L/s) | Isp (s) | TVC | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Size | Cost ($) | Mass (t) | Drag | Max Temp (K) | Tolerance | Thrust (kN) | T/W ratio | atm | vac | atm | vac | Gimbal (°) |
| File:Mk55 radial engine-t.png | Rockomax Mark 55 Radial Mount Liquid Engine | Radial Mounted | 850 | 1.5 | 0.2 | 3600 | 7 | 120 | 8.2 | 8.7 | 7.4 | 280 | 330 | 1.0 |
| File:Lv-t30 small-t.png | LV-T30 Liquid Fuel Engine | Small | 850 | 1.25 | 0.2 | 3600 | 7 | 215 | 17.5 | 13.7 | 11.8 | 320 | 370 | - |
| File:Lv-t45-t.png | LV-T45 Liquid Fuel Engine | Small | 950 | 1.5 | 0.2 | 3600 | 7 | 200 | 13.6 | 12.7 | 11.0 | 320 | 370 | 1.0 |
| File:Lv-909 small-t.png | LV-909 Liquid Fuel Engine | Small | 750 | 0.5 | 0.2 | 3600 | 7 | 50 | 10.2 | 3.4 | 2.6 | 300 | 390 | 0.5 |
| File:Toroidal aerospike-t.png | Toroidal Aerospike Rocket | Small | 850 | 1 | 0.2 | 3600 | 20 | 250 | 25.5 | 13.1 | 13.1 | 390 | 390 | - |
| File:Lv-909 large-t.png | Rockomax "Poodle" Liquid Engine | Large | 600 | 2.5 | 0.2 | 3600 | 7 | 220 | 9.0 | 16.6 | 11.5 | 270 | 390 | 2.5 |
| File:Lv-t30 large-t.png | Rockomax "Mainsail" Liquid Engine | Large | 850 | 6 | 0.2 | 3600 | 7 | 1500 | 25.5 | 109.3 | 92.7 | 280 | 330 | 1.0 |
| File:LVN.PNG | LV-N Atomic Rocket Engine | Small | 1700 | 2.25 | 0.2 | 4000 | 12 | 60 | 2.7 | 5.5 | 1.5 | 220 | 800 | 1.0 |
