Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:weapon
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:RD-0110_engine
gptkb:RD-107_engine gptkb:RD-108_engine |
| gptkbp:can_be_used_with |
gptkb:RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
LOX
|
| gptkbp:is_a |
liquid oxygen
|
| gptkbp:is_compatible_with |
gptkb:RP-1
various materials |
| gptkbp:is_known_for |
high combustion efficiency
cryogenic storage requirements high specific impulse when burned with RP-1 higher performance than solid propellants |
| gptkbp:is_often_compared_to |
liquid hydrogen
|
| gptkbp:is_part_of |
cryogenic propellant systems
oxylhydrogen engines |
| gptkbp:is_used_in |
gptkb:Saturn_V
gptkb:Delta_IV gptkb:spacecraft gptkb:NASA_rockets gptkb:New_Shepard gptkb:Vega_rocket gptkb:opera gptkb:rocket |
| gptkbp:is_vulnerable_to |
liquid nitrogen
|
| gptkbp:population |
approximately 1140 kg/m³
|
| gptkbp:produced_by |
distillation of air
liquefaction of air |
| gptkbp:storage |
cryogenic temperatures
|
| gptkbp:suitable_for |
other oxidizers in some applications
|