UDMH is often used in
hypergolic rocket fuels as a
bipropellant in combination with the oxidizer
nitrogen tetroxide and less frequently with
IRFNA (inhibited red fuming nitric acid) or
liquid oxygen. UDMH is a derivative of
hydrazine and is sometimes referred to as a hydrazine. As a fuel, it is described in specification MIL-PRF-25604 in the United States. UDMH is stable and can be kept loaded in rocket fuel systems for long periods, which makes it appealing for use in many
liquid rocket engines, despite its cost. In some applications, such as the OMS in the
Space Shuttle or
maneuvering engines,
monomethylhydrazine is used instead due to its slightly higher
specific impulse. In some kerosene-fueled rockets, UDMH functions as a starter fuel to start combustion and warm the rocket engine prior to switching to kerosene. UDMH has higher stability than hydrazine, especially at elevated temperatures, and can be used as its replacement or together in a mixture. UDMH is used in many European, Russian, Indian, and Chinese rocket designs. The Russian
SS-11 Sego (aka 8K84) ICBM,
SS-19 Stiletto (aka 15A30) ICBM,
Proton,
Kosmos-3M,
R-29RMU2 Layner,
R-36M,
Rokot (based on 15A30) and the Chinese
Long March 2 are the most notable users of UDMH (which is referred to as "heptyl" (codename from
Soviet era) by Russian engineers). The
Titan,
GSLV, and
Delta rocket families use a mixture of 50% hydrazine and 50% UDMH, called
Aerozine 50, in different stages. There is speculation that it is the fuel used in the ballistic missiles that North Korea has developed and tested in 2017. == Safety ==