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.

All labels observed (1)

Label Occurrences
Aerozine 50 canonical 17

How this entity was disambiguated

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) ⓘ
Titan II rocket ⓘ
Titan III rocket ⓘ
linked to: Titan IIIC

Titan IV rocket ⓘ
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 ⓘ
usedWithOxidizer inhibited red fuming nitric acid ⓘ
nitrogen tetroxide ⓘ

How these facts were elicited

Referenced by (17)

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 ⓘ
Titan II launch vehicle → fuel → Aerozine 50 ⓘ
Transtage → fuel → Aerozine 50 ⓘ
Titan IIIA → firstStageFuel → Aerozine 50 ⓘ
Titan IIIA → secondStageFuel → Aerozine 50 ⓘ
Titan 34D → coreStagePropellant → Aerozine 50 ⓘ
Aerojet AJ10 engine family → fuel → Aerozine 50 ⓘ
Gemini launch vehicles → fuel → Aerozine 50 ⓘ
Titan II → fuelTypeFirstStage → Aerozine 50 ⓘ
Titan II → fuelTypeSecondStage → Aerozine 50 ⓘ
Service Propulsion System → fuel → Aerozine 50 ⓘ
subject linked to: Service Propulsion System (SPS)
Titan 23G → firstStagePropellant → Aerozine 50 ⓘ