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gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Aerojet_Rocketdyne_engines
|
|
gptkbp:application
|
gptkb:spacecraft
|
|
gptkbp:check_in_time
|
up to 1,000 seconds
|
|
gptkbp:cooling_system
|
gas-generator cycle
|
|
gptkbp:developer
|
gptkb:Aerojet_Rocketdyne
$100 million
|
|
gptkbp:diameter
|
3.8 ft
|
|
gptkbp:engine
|
gas-generator
single chamber
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:first_flight
|
gptkb:1962
gptkb:2021
over 200
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
liquid hydrogen
staged combustion
3,000 K
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RL-10 A
|
|
gptkbp:is_used_by
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:United_Launch_Alliance
gptkb:NASA
|
|
gptkbp:launch_vehicle
|
gptkb:dinosaur
gptkb:Delta_IV
gptkb:spacecraft
gptkb:Titan_IV
gptkb:Atlas_I
gptkb:Titan_II
gptkb:Atlas_II
gptkb:Titan_III
gptkb:Atlas_V
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:notable_album
|
gptkb:Voyager_spacecraft
|
|
gptkbp:notable_features
|
high reliability
high efficiency
reusable components
low environmental impact
|
|
gptkbp:number_of_rooms
|
gptkb:musical
1,000 psi
|
|
gptkbp:operational_status
|
gptkb:1962
in service
|
|
gptkbp:propulsion
|
18.6
450 seconds
22,300 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:successor
|
gptkb:RL-10_B
|
|
gptkbp:used_in
|
Centaur upper stage
|
|
gptkbp:weight
|
1,200 lb
|