Difference between revisions of "Template:Stats Table Liquid Fuel Engines"
From Kerbal Space Program Wiki
(Partial updates for version 1.0: fuel use is now constant, with thrust and TWR dependent on atmospheric pressure.) |
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{| class="wikitable sortable" style=white-space:nowrap | {| class="wikitable sortable" style=white-space:nowrap | ||
|- | |- | ||
− | !colspan= | + | !colspan=8 style="background: #F9F9F9"| |
!colspan=2|{{lang | !colspan=2|{{lang | ||
− | |en=[[w: | + | |en=Thrust<br>[[w:Newton_(unit)|(kN)]] |
− | | | + | |ru=Тяга<br>[[w:ru:Ньютон_(единица_измерения)|(кН)]] |
− | | | + | |pl=Ciąg<br>[[w:pl:Niuton|(kN)]] |
− | | | + | |ko=추력<br>[[w:ko:뉴턴 (단위)|(kN)]] |
− | | | + | |zh-cn=推力<br>[[w:牛頓_(單位)|(千牛)]] |
− | | | + | |ja=推力<br>([[w:ja:ニュートン|kN]]) |
− | | | + | |de=Schub<br>[[w:de:Newton_(Einheit)|(kN)]] |
− | | | + | |es=Fuerza de empuje<br>([[w:es:Newton (unidad)|kN]]) |
− | | | + | |hr=Potisak<br>(kN) |
− | |hu=[[ | + | |hu=Tolóerő<br>[[w:hu:Newton_(mértékegység)|(kN)]] |
+ | }} | ||
+ | !colspan=2|{{lang | ||
+ | |en=[[w:Thrust-to-weight_ratio|T/W<br> ratio]] | ||
+ | |ru=[[w:ru:Тяговооружённость|Тяговооружённость]] | ||
+ | |pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik<br>T/W]] | ||
+ | |zh-cn=[[w:推力重量比|推重比]] | ||
+ | |ja=[[w:ja:推力重量比|推重比]] | ||
+ | |de=[[w:de:Schub-Gewicht-Verhältnis|SGV]] | ||
+ | |es=[[w:es:Relación empuje a peso|Relación empuje<br>a peso]] | ||
+ | |hr=Omjer potiska<br>i težine | ||
+ | |hu=[[Thrust-to-weight_ratio/hu|TWR]] | ||
}} | }} | ||
+ | || | ||
!colspan=2|{{lang | !colspan=2|{{lang | ||
|en=[[w:Specific_impulse|I<sub>sp</sub>]] [[w:Second|(s)]] | |en=[[w:Specific_impulse|I<sub>sp</sub>]] [[w:Second|(s)]] | ||
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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 | ! scope="col" width="60px" | {{lang | ||
− | |en= | + | |en=[[w:Atmosphere_(unit)|atm]] |
− | |ru= | + | |ru=[[w:ru:Атмосфера_(единица_измерения)|атм]] |
− | |pl= | + | |pl=[[w:pl:Atmosfera_fizyczna|atm]] |
− | |ko= | + | |ko=[[w:ko:기압|대기권]] |
− | |zh-cn= | + | |zh-cn=[[w:标准大气压|大气]] |
− | |ja= | + | |ja=[[w:ja:標準気圧|1気圧]] |
− | |de= | + | |de=[[w:de:Atmosphäre_(Astronomie)|atm]] |
− | |es= | + | |es=[[w:es:Atmósfera (unidad)|atm]] |
− | |hr= | + | |hr=[[w:hr:Atmosfera|atm.]] |
− | |hu= | + | |hu=[[w:hu:Atmoszféra_(mértékegység)|atm.]] |
}} | }} | ||
! scope="col" width="60px" | {{lang | ! scope="col" width="60px" | {{lang | ||
− | |en=[[w: | + | |en=[[w:Vacuum|vac]] |
− | |ru=[[ | + | |ru=[[wikipedia:ru:Вакуум|вак]] |
− | |pl=[[w:pl: | + | |pl=[[w:pl:Próżnia|vac]] |
− | |zh-cn=[[w: | + | |ko=[[w:ko:진공|진공]] |
− | |ja=[[w:ja: | + | |zh-cn=[[w:真空|真空]] |
− | |de=[[w:de: | + | |ja=[[w:ja:真空|真空]] |
− | |es=[[w:es: | + | |de=[[w:de:Vakuum|Vak.]] |
− | |hr= | + | |es=[[w:es:Vacío|Vacío]] |
− | |hu=[[ | + | |hr=[[w:hr:Vakuum|Vakuum]] |
+ | |hu=[[w:hu:Vákuum|vák.]] | ||
}} | }} | ||
! scope="col" width="60px" | {{lang | ! scope="col" width="60px" | {{lang | ||
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|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]] | |ru=[[w:ru:Атмосфера_(единица_измерения)|атм]] | ||
|pl=[[w:pl:Atmosfera_fizyczna|atm]] | |pl=[[w:pl:Atmosfera_fizyczna|atm]] | ||
− | |ko=[[w:ko:기압|대기권]]|zh-cn=[[w:标准大气压|大气]] | + | |ko=[[w:ko:기압|대기권]] |
+ | |zh-cn=[[w:标准大气压|大气]] | ||
|ja=[[w:ja:標準気圧|1気圧]] | |ja=[[w:ja:標準気圧|1気圧]] | ||
|de=[[w:de:Atmosphäre_(Astronomie)|atm]] | |de=[[w:de:Atmosphäre_(Astronomie)|atm]] | ||
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|hr=[[w:hr:Vakuum|Vakuum]] | |hr=[[w:hr:Vakuum|Vakuum]] | ||
|hu=[[w:hu:Vákuum|vák.]] | |hu=[[w:hu:Vákuum|vák.]] | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{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|(≈t/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)]] | ||
+ | |ja=推進剤[[w:ja:質量流量|流量]]([[w:Flow_measurement|≈t/s]]) | ||
+ | |de=[[w:de:Raketentreibstoff|Raketentreibstoff]] [[w:de:Massenstrom|(≈t/s)]] | ||
+ | |es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (≈t/s) | ||
+ | |hr=[[w:hr:Raketno gorivo|Raketno gorivo]] (≈t/s) | ||
+ | |hu=[[w:hu:Rakéta-hajtóanyag|Hajtóanyag]] (≈t/s) | ||
}} | }} | ||
! scope="col" width="60px" | {{lang | ! scope="col" width="60px" | {{lang | ||
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|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]] | |ru=[[w:ru:Атмосфера_(единица_измерения)|атм]] | ||
|pl=[[w:pl:Atmosfera_fizyczna|atm]] | |pl=[[w:pl:Atmosfera_fizyczna|atm]] | ||
− | |ko=[[w:ko:기압|대기권]] | + | |ko=[[w:ko:기압|대기권]]|zh-cn=[[w:标准大气压|大气]] |
− | |zh-cn=[[w:标准大气压|大气]] | ||
|ja=[[w:ja:標準気圧|1気圧]] | |ja=[[w:ja:標準気圧|1気圧]] | ||
|de=[[w:de:Atmosphäre_(Astronomie)|atm]] | |de=[[w:de:Atmosphäre_(Astronomie)|atm]] | ||
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| 650 | | 650 | ||
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| 7 | | 7 | ||
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| 290 | | 290 | ||
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|- | |- | ||
| [[File:O-10 MonoPropellant Engine.png|60x60px|center]] | | [[File:O-10 MonoPropellant Engine.png|60x60px|center]] | ||
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| [[File:Mark 55 Radial mount engine.png|60x60px|center]] | | [[File:Mark 55 Radial mount engine.png|60x60px|center]] | ||
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Revision as of 20:36, 3 May 2015
Thrust (kN) |
T/W ratio |
Isp (s) | TVC | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
atm | vac | atm | vac | Fuel (≈t/s) | atm | vac | Gimbal (°) |
LV-1R Liquid Fuel Engine | X | 650 | 0.02 | 0.2 | 3 600 | 7 | 1.793 | 2 | 9.2 | 10.2 | 0.0014 | 260 | 290 | 8 | |
O-10 MonoPropellant Engine | X | 800 | 0.09 | 0.2 | 3 600 | 7 | 20 | 22.7 | 0.007 | 220 | 290 | — | |||
Rockomax 24-77 | X | 480 | 0.09 | 0.2 | 2 000 | 7 | 13.793 | 20 | 22.7 | 0.0068 | 250 | 290 | 8.0 | ||
Rockomax Mark 55 Radial Mount Liquid Engine |
X | 800 | 0.9 | 0.2 | 3 600 | 7 | 120 | 13.6 | 0.0339 | 320 | 360 | 5.0 | |||
LV-1 Liquid Fuel Engine | Tiny | 350 | 0.03 | 0.2 | 3 600 | 7 | 4 | 13.6 | 0.0014 | 220 | 290 | — | |||
Rockomax 48-7S | Tiny | 300 | 0.1 | 0.2 | 3 600 | 7 | 30 | 30.6 | 0.0087 | 300 | 350 | 1.0 | |||
LV-909 Liquid Fuel Engine | Small | 750 | 0.5 | 0.2 | 3 600 | 7 | 50 | 10.2 | 0.0131 | 300 | 390 | 0.5 | |||
LV-T30 Liquid Fuel Engine | Small | 850 | 1.25 | 0.2 | 3 600 | 7 | 215 | 17.5 | 0.0592 | 320 | 370 | — | |||
LV-T45 Liquid Fuel Engine | Small | 950 | 1.5 | 0.2 | 3 600 | 7 | 200 | 13.6 | 0.0551 | 320 | 370 | 1.0 | |||
R.A.P.I.E.R. Engine[Note 1] | Small | 3 600 | 1.2 | 0.2 | 3 600 | 20 | 175 | 14.9 | 0.0496 | 320 | 360 | 3.0 | |||
Toroidal Aerospike Rocket | Small | 3 850 | 1.5 | 0.2 | 3 600 | 20 | 175 | 11.9 | 0.0457 | 388 | 390 | — | |||
LV-N Atomic Rocket Motor | Small | 8 700 | 2.25 | 0.2 | 4 000 | 12 | 60 | 2.7 | 0.0076 | 220 | 800 | 1.0 | |||
Rockomax "Poodle" Liquid Engine | Large | 1 600 | 2 | 0.2 | 3 600 | 7 | 220 | 11.2 | 0.0575 | 270 | 390 | 2.5 | |||
Rockomax "Skipper" Liquid Engine | Large | 2 850 | 3 | 0.2 | 3 600 | 8 | 650 | 22.1 | 0.1791 | 320 | 370 | 1.0 | |||
Rockomax "Mainsail" Liquid Engine | Large | 5 650 | 6 | 0.2 | 3 600 | 7 | 1 500 | 25.5 | 0.4247 | 320 | 360 | 1.0 | |||
LFB KR-1x2[Note 2] | Large | 16 400 (13 462.4) |
42 (10) |
0.2 | 3 600 | 20 | 2 000 | 4.9 (20.4) |
0.6002 | 290 | 340 | 0.5 | |||
Kerbodyne KR-2L Advanced Engine | Extra large | 20 850 | 6.5 | 0.2 | 3 600 | 7 | 2 500 | 39.2 | 0.6706 | 280 | 380 | 1.0 | |||
S3 KS-25x4 Engine Cluster | Extra large | 32 400 | 9.75 | 0.2 | 3 600 | 20 | 3 200 | 33.5 | 0.9061 | 320 | 360 | 0.5 |