 | RM-01 Credit - Boeing / Rocketdyne
| Fuel: Hydrazine. Fuel Density: 1.008 g/cc. Fuel Freezing Point: 2.00 deg C. Fuel Boiling Point: 113 deg C. Hydrazine (N2H4) found early use as a fuel, but it was quickly replaced by UDMH. It is still used as a monopropellant for satellite station-keeping motors. Hydrazine marketed for rocket propellant contains a minimum of 97 per cent N2H4, the other constituent being primarily water. Hydrazine is a clear, water-white, hygroscopic liquid. The solid is white. Hydrazine a toxic, flammable caustic liquid and a strong reducing agent. Its odour is similar that of ammonia, though less strong. It is slightly soluble in ammonia and methyl-amine. It is soluble in water, methanol, ethanol, UDMH, and ethylenediamine. Hydrazine is manufactured by the Raschig process, which involves the oxidation of ammonia to chloramine, either indirectly with aqueous sodium hypochlorite or directly with chlorine, and subsequent reaction of chloramine with excess ammonia. Raw materials include caustic, ammonia, and chlorine; these are high-tonnage, heavy chemicals. The cost of anhydrous hydrazine in drum quantities in 1959 was $ 7.00 per kg. The projected price, based on large-scale commercial production, was expected to be $ 1.00 per kg. Due to environmental regulations, by 1990 NASA was paying $ 17.00 per kg.
Engines Using Hydrazine
Engine
engineslink |
Thrust(vac)
kN |
Thrust(sl)
kN |
Isp
sec |
Isp (sea level)
sec |
Designed for
|
Status
|
|
RM-01
|
0.000
|
|
91
|
|
|
|
|
|
|
|
|
|
|
|
MR-508
|
0.000
|
|
502
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-510
|
0.000
|
|
600
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-509
|
0.000
|
|
502
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-512
|
0.000
|
|
502
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-501B
|
0.000
|
|
303
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-502
|
0.001
|
|
304
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 10
|
0.001
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MRM-103
|
0.001
|
|
224
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-103
|
0.001
|
|
227
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 39-2
|
0.002
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 17-6
|
0.002
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-111
|
0.004
|
|
229
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 17-12
|
0.004
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
DOT-5
|
0.005
|
|
230
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
DOK-10
|
0.010
|
|
229
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 16
|
0.020
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-50
|
0.022
|
|
228
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
DOT-25
|
0.025
|
|
235
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-106
|
0.027
|
|
232
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MRM-106
|
0.027
|
|
231
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 22-5
|
0.050
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
DOK-50
|
0.050
|
|
229
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MRE-15/OMV
|
0.089
|
|
225
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 22-2
|
0.090
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-120
|
0.090
|
|
229
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 22-16
|
0.130
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MRM-122
|
0.142
|
|
228
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 22-17
|
0.178
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
MR-107
|
0.257
|
|
236
|
|
Upper Stages
|
|
|
|
|
|
|
|
|
|
MR-104
|
0.441
|
|
239
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|
REA 20-4
|
0.556
|
|
|
|
Upper Stages
|
In Production
|
|
|
|
|
|
|
|
|