Difference between revisions of "Template:Stats Table Liquid Fuel Engines"
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− | !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: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)]]|zh-cn=[[w:火箭推进剂|推进剂]] [[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)]]|ko=[[w:ko:비추력|비추력]] [[w:ko:초 (시간)|(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)]]|zh-cn=[[w:比冲|比冲]] [[w:Second|(s)]]}} |
− | !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]]}} | + | !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]]|zh-cn=[[w:推力矢量|矢量]]}} |
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{{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)]]|ko=추력 [[w:ko:뉴턴 (단위)|(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)]]|zh-cn=推力 [[w:牛頓_(單位)|(千牛)]]}} |
− | ! 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]]|zh-cn=[[w:推力重量比|推重比]]}} |
− | ! 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:Atmosphere_(unit)|atm]]|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]|pl=[[w:pl:Atmosfera_fizyczna|atm]]|ko=[[w:ko:기압|대기권]]|zh-cn=[[w:标准大气压|大气]]}} |
− | ! 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:Vacuum|vac]]|ru=[[wikipedia:ru:Вакуум|вак]]|pl=[[w:pl:Próżnia|vac]]|ko=[[w:ko:진공|진공]]|zh-cn=[[w:真空|真空]]}} |
− | ! 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:Atmosphere_(unit)|atm]]|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]|pl=[[w:pl:Atmosfera_fizyczna|atm]]|ko=[[w:ko:기압|대기권]]|zh-cn=[[w:标准大气压|大气]]}} |
− | ! 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:Vacuum|vac]]|ru=[[wikipedia:ru:Вакуум|вак]]|pl=[[w:pl:Próżnia|vac]]|ko=[[w:ko:진공|진공]]|zh-cn=[[w:真空|真空]]}} |
− | ! 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)|(°)]]}} | + | ! 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)|(°)]]|zh-cn=[[w:Gimbal|角度]] [[w:Degree_(angle)|(°)]]}} |
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| [[File:LV-1R Liquid Fuel Engine.jpg|60x60px|center]] | | [[File:LV-1R Liquid Fuel Engine.jpg|60x60px|center]] |
Revision as of 21:17, 22 August 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 (°) |
LV-1R Liquid Fuel Engine | Radial mounted | 150 | 0.03 | 0.2 | 3600 | 7 | 1.5 | 5.1 | 0.0007 | 0.0005 | 220 | 290 | ||
Rockomax 24-77 | Radial mounted | 240 | 0.09 | 0.2 | 3600 | 7 | 20 | 22.7 | 0.0082 | 0.0068 | 250 | 300 | 1.0 | |
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 | |
LV-1 Liquid Fuel Engine | Tiny | 150 | 0.03 | 0.2 | 3600 | 7 | 1.5 | 5.1 | 0.0007 | 0.0005 | 220 | 290 | - | |
Rockomax 48-7S | Tiny | 300 | 0.1 | 0.2 | 3600 | 7 | 20 | 20.4 | 0.0068 | 0.0058 | 300 | 350 | 1.0 | |
LV-T30 Liquid Fuel Engine | Small | 850 | 1.25 | 0.2 | 3600 | 7 | 215 | 17.5 | 0.0685 | 0.0592 | 320 | 370 | - | |
LV-T45 Liquid Fuel Engine | Small | 950 | 1.5 | 0.2 | 3600 | 7 | 200 | 13.6 | 0.0637 | 0.0551 | 320 | 370 | 1.0 | |
LV-909 Liquid Fuel Engine | Small | 750 | 0.5 | 0.2 | 3600 | 7 | 50 | 10.2 | 0.0170 | 0.0131 | 300 | 390 | 0.5 | |
Toroidal Aerospike Rocket | Small | 850 | 1.5 | 0.1 | 3400 | 9 | 175 | 11.9 | 0.0460 | 0.0457 | 388 | 390 | - | |
Rockomax "Poodle" Liquid Engine | Large | 600 | 2.5 | 0.2 | 3600 | 7 | 220 | 9.0 | 0.0831 | 0.0575 | 270 | 390 | 2.5 | |
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 | |
LV-N Atomic Rocket Engine | Small | 1700 | 2.25 | 0.2 | 4000 | 12 | 60 | 2.7 | 0.0278 | 0.0076 | 220 | 800 | 1.0 |