-
Aerozine 50 is a 50:50 mix by
weight of
hydrazine and
unsymmetrical dimethylhydrazine (UDMH),
originally developed in the late 1950s by
Aerojet General...
- 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,...
-
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)...
-
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...
-
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...
-
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...
-
Laboratories (TRW) for use in the
Apollo Lunar Module descent stage. It used
Aerozine 50 fuel and
dinitrogen tetroxide (N 2O 4) oxidizer. This
engine used a...
- two-stage liquid-fuel rocket,
using a
hypergolic propellant combination of
Aerozine 50 fuel and
nitrogen tetroxide oxidizer. The
first stage was
powered by...
- URSA 25 R TRW Inc.
Aerozine 50 or MMH N2O4 111 25 URSA 100 R TRW Inc.
Aerozine 50 or MMH N2O4 445 100 URSA 200 R TRW Inc.
Aerozine 50 or MMH N2O4 890...
- the first-stage fuel tank,
causing it to leak a
cloud of its
Aerozine 50 fuel.
Aerozine 50 is
hypergolic with the
Titan II's oxidizer,
dinitrogen tetroxide...
