Lox/LNG

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
 
 
 
 
 
 
 
 
 

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