Difference between revisions of "Fuel tank"

Revision as of 17:33, 1 August 2013

A liquid fuel tank holds liquid fuel and sometimes oxidizer. Liquid fuel is required for both rocket engines and jet engines, whereas oxidizer is only used by rocket engines.

Overview

A liquid fuel tank can provide fuel to any engine directly attached to it. When tanks are directly connected together in a stack they will feed their contents from the top to the bottom of the stack. It is possible to mount additional fuel tanks radially with or without decouplers, and to transfer their contents to a central tank using fuel lines. This can be used to construct an asparagus staging system where outer tanks are drained first and dropped once empty, while still keeping the central tank full. This can be tricky to construct when dealing with very large rockets as the rocket engines of the outer layers have to be kept running long enough to ensure the rest of the rocket can get into orbit once they have stopped providing thrust.

Real world application

In real spacecraft, the liquid fuel is usually highly refined kerosene for the first stage and/or liquid hydrogen (LH2) for subsequent stages, and the oxidizer is usually liquid oxygen (LOX). Both the fuel and oxidizer are stored under slight pressure in special fuel tanks to keep them from vaporizing; this is because LH2 and LOX require temperatures below 20.28 K (−252.87 °C, −423.17 °F) and 90.19 K (−182.96 °C, −297.33 °F) respectively to remain in a liquid state. In comparison, jet aircraft carry only liquid fuel, as jet engines can rely solely on atmospheric oxygen as oxidizer. Most jet engines operate using a refined kerosene hydro-carbon, similar to diesel, which can actually be used in some diesel engines. However, it is not recommended, or legal in some places, to use jet fuel as a replacement for diesel due to its high lead content and lesser lubricating ability.

Tanks

Rocket fuel tanks

These tanks contain both liquid fuel and oxidizer and are designed for use with rocket engines. They can also be used for jet engines, however fuselage fuel tanks should be used, because they don't contain oxidizer, which is not used by jet engines. The oxidizer/liquid fuel ratio is exact except for the Oscar-B Fuel Tank.

Liquid fuel and oxidizer density are both 5 kg/unit				Mass (t)					Liquid Fuel ()	Oxidizer ()
Image	Part	Radial size	Cost ()	Full	Empty	Max. Temp. (K)	Tolerance (m/s)	Tolerance (g)
	R-4 'Dumpling' External Tank	X	50 (39.90)	0.1238	0.0138	2 000	5	50	9.9	12.1
	R-11 'Baguette' External Tank	X	50 (25.21)	0.3038	0.0338	2 000	5	50	24.3	29.7
	R-12 'Doughnut' External Tank	Small	147 (119.46)	0.3375	0.0375	2 000	6	50	27	33
	Oscar-B Fuel Tank	Tiny	70 (51.64)	0.225	0.025	2 000	6	50	18	22
	FL-T100 Fuel Tank	Small	150 (104.1)	0.5625	0.0625	2 000	6	50	45	55
	FL-T200 Fuel Tank	Small	275 (183.2)	1.125	0.125	2 000	6	50	90	110
	FL-T400 Fuel Tank	Small	500 (316.4)	2.25	0.25	2 000	6	50	180	220
	FL-T800 Fuel Tank	Small	800 (432.8)	4.5	0.5	2 000	6	50	360	440
	Rockomax X200-8 Fuel Tank	Large	800 (432.8)	4.5	0.5	2 000	6	50	360	440
	Rockomax X200-16 Fuel Tank	Large	1 550 (815.6)	9	1	2 000	6	50	720	880
	Rockomax X200-32 Fuel Tank	Large	3 000 (1 531.2)	18	2	2 000	6	50	1 440	1 760
	Rockomax Jumbo-64 Fuel Tank	Large	5 750 (2 812.4)	36	4	2 000	6	50	2 880	3 520
	Kerbodyne S3-3600 Tank	Extra large	3 250 (1 597.6)	20.25	2.25	2 000	6	50	1 620	1 980
	Kerbodyne S3-7200 Tank	Extra large	6 500 (3 195.2)	40.5	4.5	2 000	6	50	3 240	3 960
	Kerbodyne S3-14400 Tank	Extra large	13 000 (6 390.4)	81	9	2 000	6	50	6 480	7 920
	Mk2 Rocket Fuel Fuselage Short	Mk2	750 (566.4)	2.29	0.29	2 500	50	50	180	220
	Mk2 Rocket Fuel Fuselage	Mk2	1 450 (1 082.8)	4.57	0.57	2 500	50	50	360	440
	Mk3 Rocket Fuel Fuselage Short	Mk3	2 500 (1 352.5)	14.29	1.79	2 700	50	50	1 125	1 375
	Mk3 Rocket Fuel Fuselage	Mk3	5 000 (2 705)	28.57	3.57	2 700	50	50	2 250	2 750
	Mk3 Rocket Fuel Fuselage Long	Mk3	10 000 (5 410)	57.14	7.14	2 700	50	50	4 500	5 500
	C7 Brand Adapter - 2.5m to 1.25m	Small, Large	800 (433.0)	4.57	0.57	2 300	20	50	360	440
	C7 Brand Adapter Slanted - 2.5m to 1.25m	Small, Large	800 (433.0)	4.57	0.57	2 300	20	50	360	440
	Mk2 to 1.25m Adapter	Small, Mk2	550 (366.4)	2.29	0.29	2 500	50	50	180	220
	Mk2 to 1.25m Adapter Long	Small, Mk2	1 050 (682.8)	4.57	0.57	2 500	50	50	360	440
	Mk2 Bicoupler	Small, Mk2 x 2	860 (676.4)	2.29	0.29	2 500	50	50	180	220
	2.5m to Mk2 Adapter	Large, Mk2	800 (432.8)	4.57	0.57	2 500	50	50	360	440
	Mk3 to Mk2 Adapter	Mk2, Mk3	2 200 (1 282.0)	11.43	1.43	2 600	50	50	900	1 100
	Mk3 to 2.5m Adapter	Large, Mk3	2 500 (1 353.0)	14.29	1.79	2 600	50	50	1 125	1 375
	Mk3 to 2.5m Adapter Slanted	Large, Mk3	2 500 (1 353.0)	14.29	1.79	2 600	50	50	1 125	1 375
	Mk3 to 3.75m Adapter	Extra large, Mk3	2 500 (1 353.0)	14.29	1.79	2 600	50	50	1 125	1 375
	Kerbodyne ADTP-2-3	Large, Extra large	1 623 (246.0)	16.88	1.88	2 000	6	50	1 350	1 650

Jet fuel fuselages

Fuselage tanks can only be used with jet engines, as they don't contain the oxidizer required to operate rocket engines.

Liquid Fuel Density is 5 kg/unit				Mass (t)					Liquid Fuel ()
Image	Part	Radial size	Cost ()	Full	Empty	Max. Temp. (K)	Tolerance (m/s)	Tolerance (g)
	Engine Nacelle[Note 1]	Small	600 (480)	0.925	0.15	2 000	10	50	150
	Engine Pre-cooler[Note 1]	Small	1 650 (1 618)	0.375	0.15	2 000	10	50	40
	Mk1 Diverterless Supersonic Intake[Note 1]	Small	720 (560)	1.18	0.17	2 000	10	50	200
	Mk0 Liquid Fuel Fuselage	Tiny	200 (160)	0.275	0.025	2 000	10	50	50
	Mk1 Liquid Fuel Fuselage	Small	550 (230)	2.25	0.25	2 000	10	50	400
	Mk2 Liquid Fuel Fuselage Short	Mk2	750 (430)	2.29	0.29	2 500	50	50	400
	Mk2 Liquid Fuel Fuselage	Mk2	1 450 (810)	4.57	0.57	2 500	50	50	800
	Mk3 Liquid Fuel Fuselage Short	Mk3	4 300 (2 300)	14.29	1.79	2 700	50	50	2 500
	Mk3 Liquid Fuel Fuselage	Mk3	8 600 (4 600)	28.57	3.57	2 700	50	50	5 000
	Mk3 Liquid Fuel Fuselage Long	Mk3	17 200 (9 200)	57.14	7.14	2 700	50	50	10 000
	NCS Adapter	Small, Tiny	320 (256)	0.5	0.1	2 400	10	50	80
	FAT-455 Aeroplane Main Wing[Note 2]	X	2 800 (2 320)	3.78	0.78	1 200	15	50	600
	Big-S Wing Strake[Note 2]	X	1 000 (920)	0.6	0.1	2 400	15	50	100
	Big-S Delta Wing[Note 2]	X	3 000 (2 760)	2.0	0.5	2 400	15	50	300

Modder's resource

The fuel/dry/full mass of dedicated fuel tanks are associated with the following formulas. This assume that the game values are given in liters (1 L = 1 dm³ = 0.001 m³) and metric tons (1 t = 1 Mg = 1000 kg).

${\displaystyle {\text{mass}}_{\text{fuel}}=({\text{fuel}}+{\text{oxidizer}})\cdot 0.005{\frac {\text{t}}{\text{l}}}}$

${\displaystyle {\text{mass}}_{\text{dry}}={\text{mass}}_{\text{full}}-{\text{mass}}_{\text{fuel}}={\text{mass}}_{\text{full}}-({\text{fuel}}+{\text{oxidizer}})\cdot 0.005{\frac {\text{t}}{\text{l}}}}$

Take the Rockomax X200-16 Fuel Tank for example. Based on some rough in-game measurements it is approximately 0.67 meters tall with a radius of 1 meter. This would give the tank/stage a real world volume of around 2094.4 liters (2.0944 m³). Dividing the tank's actual in-game fuel capacity (0.72 m³ + 0.88 m³ = 1.6 m³) by its total volume we can find what percentage of the volume is used for fuel, around 76.39%, very close to the roughly 80% for the Saturn V's stages. The reason the entire volume is not used is because the actual fuel tank is a pressure vessel with rounded ends inside the cylindrical stage.

Notes

• Before v0.18 all fuel tanks provided fuel for both rocket engines and jet engines, because there was only one type of fuel recognized in game.

• Since v0.18 fuselages cannot be used to power rocket engines anymore, as they don't contain the necessary oxidizer.

• RCS uses monopropellant fuel that is stored in different tanks.

See also

• Reaction engine
• Jet engine
• Liquid fuel
• Oxidizer
• Liquid hydrogen on Wikipedia
• Liquid oxygen on Wikipedia
• RP-1 on Wikipedia