Difference between revisions of "Template:Stats Table Liquid Fuel Engines"

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(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=10 style="background: #F9F9F9"|
+
!colspan=8 style="background: #F9F9F9"|
 
!colspan=2|{{lang
 
!colspan=2|{{lang
|en=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(≈t/s)]]
+
|en=Thrust<br>[[w:Newton_(unit)|(kN)]]
|ru=[[wikipedia:ru:Ракетное_топливо|топливо]] [[wikipedia:ru:Расходомер|(≈t/s)]]
+
|ru=Тяга<br>[[w:ru:Ньютон_(единица_измерения)|(кН)]]
|pl=[[w:pl:Paliwo_rakietowe|Paliwo]] [[w:pl:Przepływomierz|(≈t/s)]]
+
|pl=Ciąg<br>[[w:pl:Niuton|(kN)]]
|ko=[[w:ko:로켓 연료|연료]] [[w:Flow_measurement|(≈t/s)]]
+
|ko=추력<br>[[w:ko:뉴턴 (단위)|(kN)]]
|zh-cn=[[w:火箭推进剂|推进剂]] [[w:Flow_measurement|(≈t/s)]]
+
|zh-cn=推力<br>[[w:牛頓_(單位)|(千牛)]]
|ja=推進剤[[w:ja:質量流量|流量]]([[w:Flow_measurement|≈t/s]])
+
|ja=推力<br>([[w:ja:ニュートン|kN]])
|de=[[w:de:Raketentreibstoff|Raketentreibstoff]] [[w:de:Massenstrom|(≈t/s)]]
+
|de=Schub<br>[[w:de:Newton_(Einheit)|(kN)]]
|es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (≈t/s)
+
|es=Fuerza de empuje<br>([[w:es:Newton (unidad)|kN]])
|hr=[[w:hr:Raketno gorivo|Raketno gorivo]] (≈t/s)
+
|hr=Potisak<br>(kN)
|hu=[[w:hu:Rakéta-hajtóanyag|Hajtóanyag]] (≈t/s)
+
|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=Thrust<br>[[w:Newton_(unit)|(kN)]]
+
|en=[[w:Atmosphere_(unit)|atm]]
|ru=Тяга<br>[[w:ru:Ньютон_(единица_измерения)|(кН)]]
+
|ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]
|pl=Ciąg<br>[[w:pl:Niuton|(kN)]]
+
|pl=[[w:pl:Atmosfera_fizyczna|atm]]
|ko=추력<br>[[w:ko:뉴턴 (단위)|(kN)]]
+
|ko=[[w:ko:기압|대기권]]
|zh-cn=推力<br>[[w:牛頓_(單位)|(千牛)]]
+
|zh-cn=[[w:标准大气压|大气]]
|ja=推力<br>([[w:ja:ニュートン|kN]])
+
|ja=[[w:ja:標準気圧|1気圧]]
|de=Schub<br>[[w:de:Newton_(Einheit)|(kN)]]
+
|de=[[w:de:Atmosphäre_(Astronomie)|atm]]
|es=Fuerza de empuje<br>([[w:es:Newton (unidad)|kN]])
+
|es=[[w:es:Atmósfera (unidad)|atm]]
|hr=Potisak<br>(kN)
+
|hr=[[w:hr:Atmosfera|atm.]]
|hu=Tolóerő<br>[[w:hu:Newton_(mértékegység)|(kN)]]
+
|hu=[[w:hu:Atmoszféra_(mértékegység)|atm.]]
 
}}
 
}}
 
! scope="col" width="60px" | {{lang
 
! scope="col" width="60px" | {{lang
|en=[[w:Thrust-to-weight_ratio|T/W<br> ratio]]
+
|en=[[w:Vacuum|vac]]
|ru=[[w:ru:Тяговооружённость|Тяговооружённость]]
+
|ru=[[wikipedia:ru:Вакуум|вак]]
|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik<br>T/W]]
+
|pl=[[w:pl:Próżnia|vac]]
|zh-cn=[[w:推力重量比|推重比]]
+
|ko=[[w:ko:진공|진공]]
|ja=[[w:ja:推力重量比|推重比]]
+
|zh-cn=[[w:真空|真空]]
|de=[[w:de:Schub-Gewicht-Verhältnis|SGV]]
+
|ja=[[w:ja:真空|真空]]
|es=[[w:es:Relación empuje a peso|Relación empuje<br>a peso]]
+
|de=[[w:de:Vakuum|Vak.]]
|hr=Omjer potiska<br>i težine
+
|es=[[w:es:Vacío|Vacío]]
|hu=[[Thrust-to-weight_ratio/hu|TWR]]
+
|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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{{Radial Size/Cell|X}}
 
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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
(Funds)
Mass
(t)
Drag Max. Temp.
(K)
Tolerance
(m/s)
atm vac atm vac Fuel (≈t/s) atm vac Gimbal
(°)
LV-1R Liquid Fuel Engine HD.png
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.png
O-10 MonoPropellant Engine X 800 0.09 0.2 3 600 7 20 22.7 0.007 220 290
Rockomax 24 77 Transparent.png
Rockomax 24-77 X 480 0.09 0.2 2 000 7 13.793 20 22.7 0.0068 250 290 8.0
Mark 55 Radial mount engine.png
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 HD.png
LV-1 Liquid Fuel Engine Tiny 350 0.03 0.2 3 600 7 4 13.6 0.0014 220 290
Rockomax 48-7S.png
Rockomax 48-7S Tiny 300 0.1 0.2 3 600 7 30 30.6 0.0087 300 350 1.0
LV-T909 LFE.png
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 recent.png
LV-T30 Liquid Fuel Engine Small 850 1.25 0.2 3 600 7 215 17.5 0.0592 320 370
LV-T45 LFE.png
LV-T45 Liquid Fuel Engine Small 950 1.5 0.2 3 600 7 200 13.6 0.0551 320 370 1.0
Rapier Engine 01.png
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
ToroidalAerospikeRocket.png
Toroidal Aerospike Rocket Small 3 850 1.5 0.2 3 600 20 175 11.9 0.0457 388 390
LV-N Atomic.png
LV-N Atomic Rocket Motor Small 8 700 2.25 0.2 4 000 12 60 2.7 0.0076 220 800 1.0
RockomaxPoodle.png
Rockomax "Poodle" Liquid Engine Large 1 600 2 0.2 3 600 7 220 11.2 0.0575 270 390 2.5
Skipper.png
Rockomax "Skipper" Liquid Engine Large 2 850 3 0.2 3 600 8 650 22.1 0.1791 320 370 1.0
Rockomax Mainsail transparent.png
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.png
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
Big1.png
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
Quad.png
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
  1. The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the liquid fuel engine properties are shown.
  2. The LFB KR-1x2 is a liquid fuel booster -- a combination of a "normal" engine and a fuel tank.