N2O4/UDMH
8K84 back
Credit - © Mark Wade
Propellant Formulation: N2O4/UDMH. Optimum Oxidiser to Fuel Ratio: 2.61. Temperature of Combustion: 3,415 deg K. Ratio of Specific Heats: 1.25. Density: 1.18 g/cc. Characteristic velocity c: 1,720 m/s (5,640 ft/sec). Isp Shifting: 285 sec. Isp Frozen: 273 sec. Pp Isp Shifting: 336. Isp (sl): 285. Isp (vac): 333.
Oxidiser: N2O4. Oxidiser Density: 1.450 g/cc. Oxidiser Freezing Point: -11 deg C. Oxidiser Boiling Point: 21 deg C.

Nitrogen tetroxide became the storable liquid propellant of choice from the late 1950's. Nitrogen tetroxide consists principally of the tetroxide in equilibrium with a small amount of nitrogen dioxide (NO2). The purified grade contains less than 0.1 per cent water. Nitrogen tetroxide (N2O4) has a characteristic reddish-brown colour in both liquid and gaseous phases. The solid tetroxide is colorless. N2O4 has an irritating, unpleasant acid-like odour. N2O4 is a very reactive, toxic oxidiser. It is non-flammable with air; however, it will inflame combustible materials. It is not sensitive to mechanical shock, heat, or detonation. Nitrogen dioxide is made by the catalytic oxidation of ammonia; steam is used as a diluent to reduce the combustion temperature. Most of the water is condensed out, and the gases are further cooled; the nitric oxide is oxidised to nitrogen dioxide, and the remainder of the water is removed as nitric acid. The gas is essentially pure nitrogen tetroxide, which is condensed in a brine-cooled liquefier. 1959 production amounted to 60,000 tonnes per year. In carload lots of one-ton cylinders, the price was $ 0.15 per kg. By 1990 NASA was paying $ 6.00 per kg due to environmental regulations.


Fuel: UDMH. Fuel Density: 0.793 g/cc. Fuel Freezing Point: -57 deg C. Fuel Boiling Point: 63 deg C.

Unsymmetrical Dimethylhydrazine ((CH3)2NNH2) became the storable liquid fuel of choice by the mid-1950's. Development of UDMH in the Soviet Union began in 1949. It is used in virtually all storable liquid rocket engines except for some orbital manoeuvring engines in the United States, where MMH has been preferred due to a slightly higher density and performance. Unsymmetrical dimethylhydrazine (UDMH) is 98 to 99 per cent pure and is described by Military Specification MIL-D-25604. The normally expected impurities are dimethylamine and water. UDMH is a clear, hygroscopic liquid which yellows on exposure to air. It absorbs oxygen and carbon dioxide. UDMH is a toxic volatile liquid. It exhibits the sharp ammoniacal or fishy odour which is characteristic of organic amines. It is completely miscible with water, ethanol, and most petroleum fuels. It is not shock sensitive. The vapours are flammable in air over 2.5 to 95 per cent concentration range. UDMH can be produced commercially by nitrosation of dimethylamine, to N-nitro-sodimethylrtmine, followed by reduction of the intermediate to UDMH and subsequent purification. UDMH can be prepared, also, by a modification of the Raschig process (see discussion of hydrazine), in which the chloramine intermediate is with dimethylamine rather than with ammonia. The price in 1959 for tank-car quantities was under $ 1.00 per kg. Engineering studies indicated a price of $ 1.00 per kg with large scale sustained production. But due to its toxic nature, production and transport costs soared in response to environmental regulations. By the 1980's NASA was paying $ 24.00 per kg.


Engines Using N2O4/UDMH
Engine
engineslink
Thrust(vac)
kN
Thrust(sl)
kN
Isp
sec
Isp (sea level)
sec
Designed for Status
RD-0230         Upper Stages Out of Production
RD-0209         First Stages Developed 1961-65
RD-0229         Upper Stages Out of Production
RD-0232         First Stages  
RD-0257         Upper Stages Out of Production
RD-0256         Upper Stages Out of Production
RD-0246         First Stages Design concept
RD-0250         Upper Stages Design concept
SE-1, 1-1, -2, and -4 Series            
RD-0208         First Stages Developed 1961-65
RD-0251         Upper Stages Design concept
RD-263F         First Stages Developed 1980
RDMT-0.4 X 0.000   290   Upper Stages In Production
11D431 0.006       Upper Stages In Production
RDMT-8 X 0.008   296   Upper Stages Developed 1980's
Stepanov IS/US 1 kgf 0.010       Upper Stages Out of Production
RDMT-12 0.012   279   Upper Stages In Production
17D58E 0.013   247   Upper Stages In Production
DST-25 0.025   285   Upper Stages In Production
RDMT-50 0.050   255   Upper Stages In Production
11D446 0.052       Upper Stages In Production
11D445 0.065       Upper Stages In Production
Stepanov LK/LOK 10 kgf 0.098       Upper Stages Out of Production
DST-100A 0.100   304   Upper Stages In Production
DST-100 0.100   276   Upper Stages In Production
RDMT-100 0.100   260   Upper Stages In Production
11D428 0.110       Upper Stages In Production
RDMT-135 0.135   260   Upper Stages In Production
Stepanov IS/US 16 kgf 0.157       Upper Stages Out of Production
DST-200A 0.200   300   Upper Stages In Production
DST-200 0.200   280   Upper Stages In Production
RDMT-200 0.200   255   Upper Stages In Production
SE-5-2/-3 0.205   272      
Isayev TKS attitude 0.390       Upper Stages In Production
Stepanov LK/LOK 40 kgf 0.390       Upper Stages Out of Production
11D458 0.392   252   Upper Stages In Production
RDMT-400A 0.400   290   Upper Stages Developed 1980's
RDMT-400 0.400   255   Upper Stages In Production
RDMT-400 X 0.400   296   Upper Stages Developed 1980's
DMT-600 0.600   301   Upper Stages In Production
17D61 2.943   326   Upper Stages Design 1999
KDU-426 3.089   292   Upper Stages In Production
KRD-79 3.090       Upper Stages In Production
KTDU-417-B 3.430   254   Upper Stages Out of Production
Isayev Polet/IS 3.920       Upper Stages Out of Production
RD-0225 3.923   287   Upper Stages Hardware
KRD-442 4.380       Upper Stages In Production
RD-0237 4.900   200   Upper Stages  
RD-866 5.200   306   Upper Stages Out of Production
MUT 5.635   292   Upper stages Developed 2005
RD-860 5.900   320   Upper Stages Developed 1972
NII 612 kgf 6.000   286   Upper Stages Developed
KTDU-80 6.190   302   Upper Stages In Production
RD-869 8.580   313   Upper Stages  
YF-23 11.000 10.200 282 260 Upper Stages In Production
RD-0236 15.760   293 18 Upper Stages Out of Production
11D416 16.400       Upper Stages Study 1968
KRD-61 18.800   313   Upper Stages Out of Production
KTDU-425 18.850   312   Upper Stages Out of Production
KTDU-425A 18.890   315   Upper Stages Out of Production
S5.92 19.600   327   Upper Stages In production
S5.98M 19.620   326   Upper Stages  
RD-859 20.050   312   Upper Stages Hardware
RD-858 20.100   315   Upper Stages Hardware
RD-864 20.200   309   Upper Stages Out of Production
RD-868 23.250   325   Upper Stages Developed 1983-
RD-0231 29.000   275   First Stages Out of Production
11D430 29.430   307   Upper Stages In Production
RD-0207 30.900   297   Upper Stages Developed 1961-64
RD-0214 30.980   293   Upper Stages In Production
S5.51 33.196   314   Upper Stages Hardware
11D79 44.000       Upper Stages In Production
YF-40 49.000 43.200 295 260 Upper Stages Out of production
RD-856 54.230   281   Upper Stages Out of Production
RD-69M 54.300       Second Stages Out of Production
Izotov UR-100 stage 2 vernier 58.000       Upper Stages Out of Production
Vexin A 68.600 59.500 277 240 Upper Stages  
Vexin B 75.400 66.400 251 221 First Stages Out of production
RD-854 75.500   312   Upper Stages Out of Production
RD-861G 76.453   325   Upper Stages Developed 1996-
RD-861K 77.630   330   Upper Stages Developed 2005
RD-0221 78.000   330 300 Upper Stages Developed 1965-70
RD-861 78.710   317   Upper Stages In production
Burlak Stage 2 98.000   330 230 Upper Stages Development ended 1992
Vexin C 99.100 87.300 251 221 First Stages Out of production
CZ-1C-3 107.900 97.000 287 258 Upper Stages Development ended 1988
8D725 117.000   325   Upper Stages Developed 1963-1970
Topaze 120.100 106.000 255 225 Upper Stages Out of production
RD-0242 123.600   303   First Stages Developed 1977-83
8D423 131.000   325   Upper Stages Design 1964
Izotov LK-700 131.000       Upper Stages Developed 1966-69
15D13 131.400       Upper Stages Study 1968
R6-117 132.000       Upper Stages Developed 1964-66
11D423 134.000   326   Upper Stages Development ended 1968
RD-857 137.300   330   Upper Stages Out of production
RD-862 142.630   331   Upper Stages Out of Production
RD-0245 211.000   300 280 First Stages Out of Production
RD-0217 219.000   313   First Stages Out of Production
RD-0216 219.000   313   First Stages Design 1964
11D23 230.500       Upper Stages Study 1968
RD-0235 240.000   320   Upper Stages  
4D10 255.000       Upper Stages Out of Production
RD-863 276.840   301 259 First Stages Out of Production
RD-68M 285.000       First Stages Out of Production
YF-3 294.000 266.300 287 260 Upper Stages Out of production
RD-855 328.000 285.400 292 254 First Stages Out of Production
Burlak Stage 1 360.000   320 270 First Stages Development ended 1992
RD-0233 520.000   310 285 First Stages Out of Production
RD-0234 520.000   310 285 First Stages Out of Production
RD-0203 559.000 2,000.000 311 278 First Stages Hardware
RD-0204 559.000 500.000 311 278 First Stages Hardware
8D43 559.000 599.813 316 284 First Stages Hardware
RD-0206 575.500   326   Upper Stages Developed 1961-64
RD-0210 582.100   327   Upper Stages  
RD-0211 582.100 421.900 327   Upper Stages Out of Production
RD-0213 582.100 446.000 327   Upper Stages Design 1962
RD-0205 606.400   322   Upper Stages  
RD-0212 613.000   325   Upper Stages  
RD-0244 682.000   310 280 First Stages Out of Production
Viking 2 693.000 611.600 281 248 First Stages In production
YF-22 717.800 632.700 295 260 Upper Stages In Production
Viking 2B 720.000 642.300 278 248 First Stages  
Viking 4 721.000 487.100 296 200 Upper Stages  
YF-20A 750.200 672.300 289 259 First Stages Out of production
Viking 5C 752.000 670.800 278 248 First Stages  
RD-0255 755.000       Upper Stages  
RD-0228 755.000       Upper Stages Out of Production
YF-22/23 762.000 697.400 295 270 Upper Stages Out of production
YF-22A/23A 762.000 697.400 295 270 Upper Stages Out of production
YF-25 787.400 689.300 297 260 Upper Stages In Production
Viking 4B 805.000 571.100 296 210 Upper Stages  
YF-20B 816.300 731.500 289 259 First Stages In production
RD-0243 825.800   300   First Stages Out of Production
YF-25/23 831.000 732.400 295 260 Upper Stages In production
RD-250 881.000   301 269 First Stages Out of Production
RD-252 940.500   317   Upper Stages In production
RD-262 941.000   318   Upper Stages In production
RD-263 1,155.000   318 293 First Stages Out of Production
RD-268 1,236.000 1,147.000 319 296 First Stages Out of Production
RD-273 1,238.000     296 First Stages Developed 1975-82
RD-253-11D48 1,635.000 1,474.000 316 285 First Stages  
11D43 1,642.000   316 285 First Stages Developed 1960-64
RD-254 1,716.000       Upper Stages Study 1961
RD-275 1,745.000   317 285 First Stages In Production
RD-253 1,745.000       First Stages In Production
RD-253-UR-700 1,745.000       Upper Stages Designed 1964-1968
RD-253-14D14 1,746.000 1,578.200 317 285 First Stages In production
Press Fed 200k 2,028.000 1,325.500 306 200 Upper Stages Study 1968
RD-0202 2,236.000   311 278 First Stages  
8D43 + 11D43 2,247.450 1,980.000 310 280 First Stages Design 1962
RD-0215 2,450.000   310 280 First Stages Developed 1962-65
RD-251 2,643.000 2,366.000 301 269 First Stages In production
RD-261 3,032.000   301 270 First Stages In production
RD-264 4,521.000   318 293 First Stages  
RD-274 4,952.000     296 First Stages Developed 1975-85
RD-270 6,713.000 6,272.000 322 301 First Stages Development ended 1968
Press Fed 1000k 9,793.200 7,834.500 300 240 Upper Stages Study 1968
PF N204/UDMH-2165k 21,232.000   267 245 First Stages Study 1967
PF N204/UDMH-2912k 28,552.000   267 245 First Stages Study 1967
Press Fed 5748k 56,368.000 51,723.200 267 245 First Stages Study 1968
 
 
 
 
 
 
 
 
 

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