Aerozine 50

E570819

Aerozine 50 is a hypergolic liquid rocket propellant consisting of a 50/50 mixture of hydrazine and unsymmetrical dimethylhydrazine, valued for its storability and reliable ignition in space launch and missile systems.

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All labels observed (1)

Label Occurrences
Aerozine 50 canonical 4

Statements (45)

Predicate Object
instanceOf liquid rocket fuel
rocket propellant
developedFor U.S. missile programs
fuelType bipropellant fuel component
hasAdvantage restart capability in space
simplified engine design due to hypergolic ignition
hasAlternative hydrazine
monomethylhydrazine
unsymmetrical dimethylhydrazine
hasComponent hydrazine
unsymmetrical dimethylhydrazine
hasDisadvantage environmental toxicity
handling hazards
hasProperty carcinogenic
corrosive
good density for compact tanks
highly reactive
ignites on contact with oxidizer
long-term storability
pressure-fed system compatibility
reliable ignition
room-temperature liquid
storable at ambient temperature
toxic
isHypergolicWith nitrogen tetroxide
isReplacedBy less toxic propellants in some modern systems
isUsedIn Gemini launch vehicle (Titan II GLV) NERFINISHED
Titan II rocket NERFINISHED
Titan III rocket NERFINISHED
Titan IV rocket NERFINISHED
missile systems
space launch vehicles
spacecraft propulsion systems
upper stages of rockets
various ICBMs
mixtureRatioByVolume 50% hydrazine
50% unsymmetrical dimethylhydrazine
namingOrigin derived from 'aero' and 'hydrazine' with 50 indicating 50/50 mixture
requires protective equipment for handling
specialized storage systems
safetyClassification highly hazardous material
usedBy United States Air Force
usedInEra Cold War NERFINISHED
usedWithOxidizer inhibited red fuming nitric acid
nitrogen tetroxide

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.

LR-91 fuel Aerozine 50
Service Propulsion System fuel Aerozine 50
Titan II ICBM fuel Aerozine 50