|
gptkbp:instanceOf
|
gptkb:rocket_propellant
|
|
gptkbp:alternativeTo
|
UDMH
pure hydrazine
|
|
gptkbp:appearance
|
clear, colorless liquid
|
|
gptkbp:CASNumber
|
N/A (mixture)
|
|
gptkbp:component
|
hydrazine
unsymmetrical dimethylhydrazine
|
|
gptkbp:density
|
0.87 g/cm³
|
|
gptkbp:developedBy
|
gptkb:Aerojet
|
|
gptkbp:flammability
|
highly flammable
|
|
gptkbp:ignition
|
hypergolic with oxidizer
|
|
gptkbp:introduced
|
1950s
|
|
gptkbp:mixtureRatio
|
50% hydrazine, 50% UDMH
|
|
gptkbp:storage
|
storable at room temperature
|
|
gptkbp:toxicity
|
highly toxic
|
|
gptkbp:type
|
hypergolic propellant
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:United_States_Air_Force
|
|
gptkbp:usedFor
|
gptkb:satellite
gptkb:dinitrogen_tetroxide
missile propulsion
|
|
gptkbp:usedIn
|
gptkb:satellite
gptkb:Apollo_Service_Module
gptkb:Gemini_launch_vehicle
gptkb:Titan_III_rocket
gptkb:Titan_II_rocket
gptkb:Titan_IV_rocket
|
|
gptkbp:bfsParent
|
gptkb:Apollo_Lunar_Module_Descent_Engine
gptkb:Titan_II
gptkb:Titan_IV
gptkb:Aerozine_50/Nitrogen_tetroxide
gptkb:LGM-25C_Titan_II_ICBM
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aerozine 50
|