propellantMass

P67133 predicate

Indicates the amount of propellant associated with or used by an object or system in a given context.

Observed surface forms (1)

Sample triples (16)

Subject Object
AJ-60 series approximately 40 metric tons (AJ-60A)
Dawn 425 kg via predicate surface "xenonPropellantMass"
L110 liquid core stage 110 metric tons
L110 liquid core stage 110000 kilograms
Orion 38 approximately 770 kg
S-IC about 2038000 kg
Saturn V S-II second stage about 456,000 kg
Saturn V first stage (S-IC) about 2,000,000 kilograms
Saturn V first stage (S-IC) about 4,400,000 pounds
Star 48BV upper stage
surface form: Star 48BV
approximately 2000 kg
Universal Rocket Module URM-1 about 125000 kg
Vikram 845 kg
Zefiro 23 about 23 metric tons
Zefiro 23 approximately 23000 kilograms
Zefiro 9 about 9.7 tonnes
Zefiro 9 approximately 10 tonnes