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

Revision as of 20:36, 3 May 2015

Part	Radial size	Cost ()	Mass (t)	Drag	Max. Temp. (K)	Tolerance (m/s)	atm	vac	atm	vac	Fuel (≈t/s)	atm	vac	Gimbal (°)
							Thrust (kN)		T/W ratio			I_sp (s)		TVC
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

↑ 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.
↑ The LFB KR-1x2 is a liquid fuel booster -- a combination of a "normal" engine and a fuel tank.

[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.

[Note 1]

[Note 2]

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

Revision as of 20:36, 3 May 2015

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@@ Line 1: / Line 1: @@
 {| class="wikitable sortable" style=white-space:nowrap
 |-
-!colspan=10 style="background: #F9F9F9"|
+!colspan=8 style="background: #F9F9F9"|
 !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
 |en=[[w:Specific_impulse|I<sub>sp</sub>]] [[w:Second|(s)]]
@@ Line 41: / Line 53: @@
 {{Stats Table Header|s|m|d|t|m}}
 ! 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
-|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
@@ Line 67: / Line 80: @@
 |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]]
+|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]]
 |de=[[w:de:Atmosphäre_(Astronomie)|atm]]
@@ Line 85: / Line 99: @@
 |hr=[[w:hr:Vakuum|Vakuum]]
 |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
@@ Line 90: / Line 116: @@
 |ru=[[w:ru:Атмосфера_(единица_измерения)|атм]]
 |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]]
 |de=[[w:de:Atmosphäre_(Astronomie)|atm]]
@@ Line 127: / Line 152: @@
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