Difference between revisions of "Template:Stats Table Liquid Fuel Engines"
From Kerbal Space Program Wiki
(Added skipper img) |
|||
| Line 2: | Line 2: | ||
|- | |- | ||
!colspan=10 style="background: #F9F9F9"| | !colspan=10 style="background: #F9F9F9"| | ||
| − | !colspan=2|{{lang|en=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(≈t/s)]]|ru=[[wikipedia:ru:Ракетное_топливо|топливо]] [[wikipedia:ru:Расходомер|(≈t/s)]]|pl=[[w:pl:Paliwo_rakietowe|Paliwo]] [[w:pl:Przepływomierz|(L/s)]]}} | + | !colspan=2|{{lang|en=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(≈t/s)]]|ru=[[wikipedia:ru:Ракетное_топливо|топливо]] [[wikipedia:ru:Расходомер|(≈t/s)]]|pl=[[w:pl:Paliwo_rakietowe|Paliwo]] [[w:pl:Przepływomierz|(L/s)]]|ko=[[w:ko:로켓 연료|연료]] [[w:Flow_measurement|(≈t/s)]]}} |
| − | !colspan=2|{{lang|en=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]|pl=[[w:pl:Impuls_właściwy|Isp]] [[w:pl:Sekunda|(s)]]}} | + | !colspan=2|{{lang|en=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]|pl=[[w:pl:Impuls_właściwy|Isp]] [[w:pl:Sekunda|(s)]]|ko=[[w:ko:비추력|비추력]] [[w:ko:초 (시간)|(s)]]}} |
| − | !colspan=1|{{lang|en=[[w:Thrust_Vectoring|TVC]]|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]]|pl=[[w:pl:Ciąg_wektorowany|TVC]]}} | + | !colspan=1|{{lang|en=[[w:Thrust_Vectoring|TVC]]|ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]]|pl=[[w:pl:Ciąg_wektorowany|TVC]]|ko=[[w:ko:추력편향|추력편향]]}} |
|- | |- | ||
{{Stats Table Header|s|m|d|t|m}} | {{Stats Table Header|s|m|d|t|m}} | ||
| − | ! scope="col" width="60px" | {{lang|en=Thrust [[w:Newton_(unit)|(kN)]]|ru=Тяга [[w:ru:Ньютон_(единица_измерения)|(кН)]]|pl=Ciąg [[w:pl:Niuton|(kN)]]}} | + | ! scope="col" width="60px" | {{lang|en=Thrust [[w:Newton_(unit)|(kN)]]|ru=Тяга [[w:ru:Ньютон_(единица_измерения)|(кН)]]|pl=Ciąg [[w:pl:Niuton|(kN)]]|ko=추력 [[w:ko:뉴턴 (단위)|(kN)]]}} |
! scope="col" width="60px" | {{lang|en=[[w:Thrust-to-weight_ratio|T/W ratio]]|ru=[[w:ru:Тяговооружённость|Тяговооружённость]]|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]}} | ! scope="col" width="60px" | {{lang|en=[[w:Thrust-to-weight_ratio|T/W ratio]]|ru=[[w:ru:Тяговооружённость|Тяговооружённость]]|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]}} | ||
| − | ! scope="col" width="60px" | {{lang|en=[[w:Atmosphere_(unit)|atm]]|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]|pl=[[w:pl:Atmosfera_fizyczna|atm]]}} | + | ! 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]]}} |
| − | ! scope="col" width="60px" | {{lang|en=[[w:Vacuum|vac]]|ru=[[wikipedia:ru:Вакуум|вак]]|pl=[[w:pl:Próżnia|vac]]}} | + | ! scope="col" width="60px" | {{lang|en=[[w:Vacuum|vac]]|ru=[[wikipedia:ru:Вакуум|вак]]|pl=[[w:pl:Próżnia|vac]]|ko=[[w:ko:진공|진공]]}} |
| − | ! scope="col" width="60px" | {{lang|en=[[w:Atmosphere_(unit)|atm]]|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]|pl=[[w:pl:Atmosfera_fizyczna|atm]]}} | + | ! 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]]}} |
| − | ! scope="col" width="60px" | {{lang|en=[[w:Vacuum|vac]]|ru=[[wikipedia:ru:Вакуум|вак]]|pl=[[w:pl:Próżnia|vac]]}} | + | ! scope="col" width="60px" | {{lang|en=[[w:Vacuum|vac]]|ru=[[wikipedia:ru:Вакуум|вак]]|pl=[[w:pl:Próżnia|vac]]|ko=[[w:ko:진공|진공]]}} |
| − | ! 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)|(°)]]}} | + | ! 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)|(°)]]}} |
|- | |- | ||
| [[Image:Rockomax_mark_55_radial_mount_liquid_engine.jpg|60x60px|]] | | [[Image:Rockomax_mark_55_radial_mount_liquid_engine.jpg|60x60px|]] | ||
Revision as of 03:58, 11 June 2013
| Fuel (≈t/s) | Isp (s) | TVC | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Radial size | Cost (  ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Thrust (kN) | T/W ratio | atm | vac | atm | vac | Gimbal (°) |
| File:Rockomax mark 55 radial mount liquid engine.jpg | Rockomax Mark 55 Radial Mount Liquid Engine | Radial mounted | 850 | 0.9 | 0.2 | 3600 | 7 | 120 | 13.6 | 0.0422 | 0.0382 | 290 | 320 | 3.0 |
| File:Lv-t30 liquid fuel engine.jpg | LV-T30 Liquid Fuel Engine | Small | 850 | 1.25 | 0.2 | 3600 | 7 | 215 | 17.5 | 0.0685 | 0.0592 | 320 | 370 | - |
| File:Lv-t45 liquid fuel engine.jpg | LV-T45 Liquid Fuel Engine | Small | 950 | 1.5 | 0.2 | 3600 | 7 | 200 | 13.6 | 0.0637 | 0.0551 | 320 | 370 | 1.0 |
| File:Lv-909 liquid fuel engine.jpg | LV-909 Liquid Fuel Engine | Small | 750 | 0.5 | 0.2 | 3600 | 7 | 50 | 10.2 | 0.0170 | 0.0131 | 300 | 390 | 0.5 |
| File:Toroidal aerospike-t.png | Toroidal Aerospike Rocket | Small | 850 | 1.5 | 0.1 | 3400 | 9 | 175 | 11.9 | 0.0460 | 0.0457 | 388 | 390 | - |
| File:Rockomax poodle liquid engine.jpg | Rockomax "Poodle" Liquid Engine | Large | 600 | 2.5 | 0.2 | 3600 | 7 | 220 | 9.0 | 0.0831 | 0.0575 | 270 | 390 | 2.5 |
| File:Rockomax mainfail liquid engine.jpg | Rockomax "Mainsail" Liquid Engine | Large | 850 | 6 | 0.2 | 3600 | 7 | 1500 | 25.5 | 0.5461 | 0.4633 | 280 | 330 | 1.0 |
|
Rockomax "Skipper" Liquid Engine | Large | 850 | 4 | 0.2 | 3600 | 8 | 650 | 16.6 | 0.2208 | 0.1893 | 300 | 350 | 1.0 |
| File:LVN.PNG | LV-N Atomic Rocket Engine | Small | 1700 | 2.25 | 0.2 | 4000 | 12 | 60 | 2.7 | 0.0278 | 0.0076 | 220 | 800 | 1.0 |
| File:Rockomax 24-77.jpg | Rockomax 24-77 | Radial mounted | 240 | 0.09 | 0.2 | 3600 | 7 | 20 | 22.7 | 0.0082 | 0.0068 | 250 | 300 | 1.0 |
| File:Lv-1 liquid fuel engine.jpg | LV-1 Liquid Fuel Engine | Tiny | 150 | 0.03 | 0.2 | 3600 | 7 | 1.5 | 5.1 | 0.0007 | 0.0005 | 220 | 290 | - |
