Difference between revisions of "Template:Stats Table Liquid Fuel Engines"
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|ko=[[w:ko:로켓 연료|연료]] [[w:Flow_measurement|(≈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)]] | |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)]] | |de=[[w:de:Raketentreibstoff|Raketentreibstoff]] [[w:de:Massenstrom|(≈t/s)]] | ||
|es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (≈t/s) | |es=[[w:es:Propelente#Propulsión de cohetes|Combustible]] (≈t/s) | ||
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|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]]] | ||
|de=[[w:de:Atmosphäre_(Astronomie)|atm]] | |de=[[w:de:Atmosphäre_(Astronomie)|atm]] | ||
|es=[[w:es:Atmósfera (unidad)|atm]] | |es=[[w:es:Atmósfera (unidad)|atm]] | ||
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|ko=[[w:ko:짐벌|짐벌]] [[w:ko:도 (각도)|(°)]] | |ko=[[w:ko:짐벌|짐벌]] [[w:ko:도 (각도)|(°)]] | ||
|zh-cn=[[w:Gimbal|角度]] [[w:Degree_(angle)|(°)]] | |zh-cn=[[w:Gimbal|角度]] [[w:Degree_(angle)|(°)]] | ||
− | |ja= | + | |ja=角度(°) |
|de=[[w:de:Schubvektorsteuerung|Schub­vek­tor­steu­er­ung]] [[w:de:Grad_(Winkel)|(°)]] | |de=[[w:de:Schubvektorsteuerung|Schub­vek­tor­steu­er­ung]] [[w:de:Grad_(Winkel)|(°)]] | ||
|es=[[w:es:Gimbal|Gimbal]] ([[w:es:Grado sexagesimal|º]]) | |es=[[w:es:Gimbal|Gimbal]] ([[w:es:Grado sexagesimal|º]]) |
Revision as of 12:25, 9 September 2014
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 | 650 | 0.03 | 0.2 | 3600 | 7 | 4 | 13.6 | 0.0019 | 0.0014 | 220 | 290 | - | |
O-10 MonoPropellant Engine | Radial mounted | 800 | 0.09 | 0.2 | 3600 | 7 | 20 | 22.7 | 0.0092 | 0.007 | 220 | 290 | - | |
Rockomax 24-77 | Radial mounted | 480 | 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 | 350 | 0.03 | 0.2 | 3600 | 7 | 4 | 13.6 | 0.0019 | 0.0014 | 220 | 290 | - | |
Rockomax 48-7S | Tiny | 300 | 0.1 | 0.2 | 3600 | 7 | 30 | 30.6 | 0.0102 | 0.0087 | 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 | |
R.A.P.I.E.R. Engine[Note 1] | Small | 3600 | 1.2 | 0.2 | 3600 | 20 | 175 | 14.9 | 0.0558 | 0.0496 | 320 | 360 | 3.0 | |
Toroidal Aerospike Rocket | Small | 3850 | 1.5 | 0.2 | 3600 | 20 | 175 | 11.9 | 0.0460 | 0.0457 | 388 | 390 | - | |
Rockomax "Poodle" Liquid Engine | Large | 1600 | 2 | 0.2 | 3600 | 7 | 220 | 11.2 | 0.0831 | 0.0575 | 270 | 390 | 2.5 | |
Rockomax "Mainsail" Liquid Engine | Large | 5650 | 6 | 0.2 | 3600 | 7 | 1500 | 25.5 | 0.4778 | 0.4247 | 320 | 360 | 1.0 | |
Rockomax "Skipper" Liquid Engine | Large | 2850 | 3 | 0.2 | 3600 | 8 | 650 | 22.1 | 0.2071 | 0.1791 | 320 | 370 | 1.0 | |
LV-N Atomic Rocket Motor | Small | 8700 | 2.25 | 0.2 | 4000 | 12 | 60 | 2.7 | 0.0278 | 0.0076 | 220 | 800 | 1.0 | |
LFB KR-1x2[Note 2] | Large | 16400 | 10 | 0.2 | 3600 | 20 | 2000 | 20.4 | 0.7037 | 0.6002 | 290 | 340 | 0.5 | |
Kerbodyne KR-2L Advanced Engine | Extra large | 20850 | 6.5 | 0.2 | 3600 | 7 | 2500 | 39.2 | 0.9101 | 0.6706 | 280 | 380 | 1.0 | |
S3 KS-25x4 Engine Cluster | Extra large | 32400 | 9.75 | 0.2 | 3600 | 20 | 3200 | 33.5 | 1.0194 | 0.9061 | 320 | 360 | 0.5 |