Statements (51)
Predicate | Object |
---|---|
gptkbp:instanceOf |
rocket engine
|
gptkbp:application |
satellite launch
|
gptkbp:barrelLength |
20 MPa
|
gptkbp:built |
overcame significant engineering challenges
|
gptkbp:campusFacilities |
collaborated with universities
|
gptkbp:chemicalFormula |
liquid oxygen
|
gptkbp:climate |
up to 3,000 K
|
gptkbp:collaborations |
various aerospace companies
involved in international space missions |
gptkbp:community_engagement |
engaged with aerospace community
|
gptkbp:community_outreach |
conducted educational outreach programs
|
gptkbp:competitors |
RD-180 engine
high demand in commercial spaceflight |
gptkbp:construction_cost |
estimated at $50 million
|
gptkbp:controls |
digital control system
|
gptkbp:coolingSystem |
regenerative cooling
|
gptkbp:design_feature |
multiple design iterations completed
|
gptkbp:diameter |
1.5 m
|
gptkbp:documentType |
bell nozzle
|
gptkbp:environmental_impact |
low emissions
|
gptkbp:facilities |
gptkb:NASA_Marshall_Space_Flight_Center
|
gptkbp:firstFlight |
2000
|
gptkbp:fuel_capacity |
high efficiency
|
gptkbp:fuelType |
gas-generator cycle
kerosene pyrotechnic ignition |
gptkbp:funding |
funded by government and private sectors
|
gptkbp:future_plans |
5 years
|
gptkbp:futurePlans |
planned upgrades for performance
|
gptkbp:historical_significance |
part of modern space exploration efforts
|
https://www.w3.org/2000/01/rdf-schema#label |
RD-600 engine
|
gptkbp:is_designed_to |
Aerojet Rocketdyne
|
gptkbp:is_used_in |
launch vehicles
|
gptkbp:launchDate |
high frequency planned
|
gptkbp:launchSite |
various launch sites worldwide
|
gptkbp:length |
4.5 m
|
gptkbp:lifespan |
10 years
|
gptkbp:missions |
planned for upcoming space missions
|
gptkbp:number_of_stages |
multiple
|
gptkbp:operationalHistory |
used in various missions
|
gptkbp:patentCitation |
multiple patents filed
|
gptkbp:performance |
meets industry standards
|
gptkbp:propulsion |
yes
300 seconds 600 kN |
gptkbp:public_perception |
positive feedback from industry experts
|
gptkbp:reliability |
designed for reusability
|
gptkbp:safety_features |
multiple redundant systems
|
gptkbp:status |
in development
|
gptkbp:technology |
available for research purposes
|
gptkbp:weight |
1,500 kg
|