-
Aerozine 50 is a 50:50 mix by
weight of
hydrazine and
unsymmetrical dimethylhydrazine (UDMH),
developed in the late 1950s by
Aerojet General Corporation...
-
critical usage of this
engine during the
Apollo program. This
version used
Aerozine 50 (a 1:1 mix of UDMH and hydrazine) as fuel and
nitrogen tetroxide (N2O4)...
-
propellant combinations:
liquid oxygen/RP-1,
nitrogen tetroxide (NTO)/
Aerozine 50 (a 50:50
mixture by m**** of
hydrazine and UDMH), and
liquid oxygen/liquid...
- RCS thrusters:
Sixteen × 100 lbf (440 N) in four
quads RCS propellants:
Aerozine 50 fuel /
Dinitrogen tetroxide (N2O4)
oxidizer RCS
specific impulse: 290 s...
- Bell
Aerosystems for use in the
Apollo Lunar Module ascent stage. It used
Aerozine 50 fuel, and N 2O 4 oxidizer.
Rocketdyne provided the
injector system,...
- LGM-25C, the
Titan II was the
largest USAF
missile at the time and
burned Aerozine 50 and
nitrogen tetroxide (NTO)
rather than RP-1 and LOX. The
Titan III...
- two-stage liquid-fuel rocket,
using a
hypergolic propellant combination of
Aerozine 50 fuel and
nitrogen tetroxide oxidizer. The
first stage was
powered by...
-
Titan I, the
models that
propelled the
Titan II and
later were
switched to
Aerozine 50/N2O4. This
engine was
vacuum optimized and ran the gas-generator cycle...
-
Module ascent stage or both made no
visible flame. The
Lunar Modules used
Aerozine 50 (fuel) and
dinitrogen tetroxide (oxidizer) propellants,
chosen for simplicity...
-
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...
