RL10 family

GPTKB entity

Statements (62)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application gptkb:space_mission
satellite launches
interplanetary missions
gptkbp:combustor_type gas-generator cycle
gptkbp:designed_by gptkb:Aerojet_Rocketdyne
gptkbp:first_flight gptkb:1962
gptkbp:fuel_type liquid hydrogen
https://www.w3.org/2000/01/rdf-schema#label RL10 family
gptkbp:notable_mission gptkb:New_Horizons
gptkb:James_Webb_Space_Telescope
gptkb:Orion_spacecraft
gptkb:Juno_spacecraft
gptkb:Mars_Science_Laboratory
gptkb:Hubble_Space_Telescope
gptkb:Lunar_Gateway
gptkb:Mercury_missions
gptkb:Parker_Solar_Probe
gptkb:Mars_missions
gptkb:Voyager_spacecraft
gptkb:Earth_observation
gptkb:Titan_missions
gptkb:GPS_satellites
gptkb:Iridium_satellites
International Space Station resupply
space telescopes
sample return missions
commercial satellite launches
military satellites
lunar missions
weather satellites
asteroid missions
planetary exploration missions
interstellar missions
comet missions
telecommunications satellites
Pluto missions
scientific research satellites
Venus missions
Callisto missions
Ceres missions
Enceladus missions
Europa missions
Ganymede missions
Kuiper Belt missions
Oort Cloud missions
Vesta missions
gptkbp:oxidation_states liquid oxygen
gptkbp:production_status in production
gptkbp:propulsion 22,000 lbf
gptkbp:specific_impulse 450 seconds
gptkbp:used_in gptkb:Atlas_V_upper_stage
gptkb:Delta_IV_upper_stage
Centaur upper stage
upper stages of rockets
gptkbp:variant gptkb:RL10_C-1
gptkb:RL10_A-3
gptkb:RL10_B-2
gptkbp:weight 1,200 lb
gptkbp:bfsParent gptkb:RL10-CE3
gptkb:RL10-CE4
gptkbp:bfsLayer 6