|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Titan_IIIA
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:check_in_time
|
approximately 150 seconds
|
|
gptkbp:controls
|
manual and automatic
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:developer
|
gptkb:NASA
1960s
|
|
gptkbp:emissions_standard
|
bell nozzle
|
|
gptkbp:engine
|
gptkb:NASA_Marshall_Space_Flight_Center
gptkb:spacecraft
gptkb:stock_market_index
high
ongoing
advanced
extensive
limited
notable
innovative
modular
high efficiency
influential
vertical
well-documented
documented
detailed
staged combustion
RD-0211
150 k N
RD series
vertical mount
|
|
gptkbp:engine_type
|
few
liquid bipropellant
gas generator
|
|
gptkbp:first_flight
|
gptkb:1966
|
|
gptkbp:first_introduced
|
gptkb:software
|
|
gptkbp:fuel_capacity
|
2.5 m
1.1 m
|
|
gptkbp:fuel_type
|
gptkb:RP-1
gas-generator cycle
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rocketdyne RD-0210
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:inspired_by
|
RD-0105
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:is_used_by
|
gptkb:United_States
|
|
gptkbp:maintenance
|
routine
|
|
gptkbp:manufacturer
|
gptkb:Rocketdyne
|
|
gptkbp:mission
|
gptkb:Apollo_7
|
|
gptkbp:number_of_rooms
|
single chamber
6.9 M Pa
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:propulsion
|
300 seconds
150 k N
500 N/kg
|
|
gptkbp:social_structure
|
gptkb:LOX
liquid oxygen
|
|
gptkbp:successor
|
RD-0211
|
|
gptkbp:used_in
|
gptkb:Saturn_IB
|
|
gptkbp:weight
|
approximately 300 kg
|