Aerozine 50 and nitrogen tetroxide
GPTKB entity
Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:rocket_propellant_combination
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| gptkbp:isHypergolic |
true
|
| gptkbp:notableFeature |
storable at room temperature
ignites on contact |
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:usedFor |
gptkb:satellite
missile propulsion |
| gptkbp:usedIn |
gptkb:Gemini_launch_vehicle
gptkb:Delta_II_second_stage gptkb:Viking_lander gptkb:Titan_II_missile Apollo Lunar Module Descent Propulsion System |
| gptkbp:bfsParent |
gptkb:Lunar_Module_Ascent_Stage
gptkb:Titan_II_missile gptkb:Titan_II_missile_program |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aerozine 50 and nitrogen tetroxide
|