Oxidiser: LOX. Oxidiser Density: 1.140 g/cc. Oxidiser Freezing Point: -219 deg C. Oxidiser Boiling Point: -183 deg C. Liquid oxygen was the earliest, cheapest, safest, and eventually the preferred oxidiser for large space launchers. Its main drawback is that it is moderately cryogenic, and therefore not suitable for military uses where storage of the fuelled missile and quick launch are required. Liquid oxygen, as normally supplied, is of 99.5 percent purity and is covered in the United States by Military Specification MIL-P-25508. High purity liquid oxygen has a light blue colour and is transparent. It has no characteristic odour. Liquid oxygen does not burn, but will support combustion vigorously. The liquid is stable; however, mixtures of fuel and liquid oxygen are shock-sensitive. Gaseous oxygen can form mixtures with fuel vapours that can be exploded by static electricity, electric spark, or flame. Liquid oxygen is obtained from air by fractional distillation. The 1959 United. States production of high-purity oxygen was estimated at nearly 2 million tonnes. The cost of liquid oxygen, at that time, ex-works, was $ 0.04 per kg. By the 1980's NASA was paying $ 0.08 per kg. Fuel: LNG. Liquefied natural gas - mainly methane,with traces of sulfur, etc.
Engines Using Lox/LNG
Engine
engineslink |
Thrust(vac)
kN |
Thrust(sl)
kN |
Isp
sec |
Isp (sea level)
sec |
Designed for
|
Status
|
|
RD-0149
|
49.000
|
|
370
|
|
Upper Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-56M LNG
|
73.500
|
|
|
|
Upper Stages
|
Developed 1996-
|
|
|
|
|
|
|
|
|
RD-0132M
|
98.000
|
|
|
|
Upper Stages
|
Design concept 1998-
|
|
|
|
|
|
|
|
|
RD-0145
|
147.000
|
|
374
|
|
Upper Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-0144
|
147.000
|
|
374
|
|
Upper Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-0110MD
|
245.000
|
|
|
|
Upper Stages
|
Developed 1994-on
|
|
|
|
|
|
|
|
|
RD-0143
|
343.000
|
|
372
|
|
Upper Stages
|
Design concept 1998-
|
|
|
|
|
|
|
|
|
RD-0143A
|
343.000
|
|
370
|
|
First Stages
|
Design concept 1998-
|
|
|
|
|
|
|
|
|
RD-182M
|
882.000
|
|
|
|
First Stages
|
Developed 1998-
|
|
|
|
|
|
|
|
|
RD-0229M
|
883.000
|
|
|
|
First Stages
|
Developed 1997
|
|
|
|
|
|
|
|
|
RD-0134
|
2,038.000
|
|
358
|
316
|
First Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-0139
|
2,038.000
|
|
341
|
301
|
First Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-0140
|
2,086.000
|
|
349
|
300
|
Upper Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-0141
|
2,251.000
|
|
353
|
323
|
First Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|
RD-0142
|
2,353.000
|
|
369
|
|
Upper Stages
|
Developed 1998-on
|
|
|
|
|
|
|
|
|