|
gptkbp:instance_of
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gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Space_Launch_System
|
|
gptkbp:challenges
|
overcoming thermal stresses
|
|
gptkbp:collaboration
|
gptkb:National_Academy_of_Sciences
limited
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:community_engagement
|
outreach programs
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:design_purpose
|
high efficiency
|
|
gptkbp:developed_by
|
gptkb:ISRO
|
|
gptkbp:development
|
gptkb:1990
|
|
gptkbp:development_cost
|
approximately $10 million
|
|
gptkbp:educational_value
|
inspired students in aerospace engineering
|
|
gptkbp:engine
|
staged combustion cycle
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:facilities
|
gptkb:ISRO_Propulsion_Complex
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:fuel_capacity
|
around 3 meters
around 1 meter
|
|
gptkbp:fuel_type
|
liquid propellant
kerosene
|
|
gptkbp:future_plans
|
upgraded versions
|
|
gptkbp:future_prospects
|
next-generation engines
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
ISRO's Kestrel engine
|
|
gptkbp:ignition_system
|
hypergolic ignition
|
|
gptkbp:inspiration
|
inspired by global technologies
|
|
gptkbp:integration
|
integrated with launch vehicles
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:investment
|
around 50 bar
|
|
gptkbp:is_tested_for
|
multiple test firings
|
|
gptkbp:launch_date
|
multiple launches per year
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:material
|
high-strength alloys
|
|
gptkbp:mission
|
gptkb:GSLV
gptkb:PSLV
high success rate
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:performance
|
high reliability
|
|
gptkbp:propulsion
|
around 70 k N
greater than 200
|
|
gptkbp:public_awareness
|
increased public interest
|
|
gptkbp:publications
|
numerous research papers
|
|
gptkbp:research_focus
|
advanced propulsion technologies
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:successor
|
Kestrel-2
|
|
gptkbp:training_programs
|
engineer training programs
|
|
gptkbp:used_in
|
launch vehicles
|
|
gptkbp:weight
|
approximately 300 kg
|
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
|
|
gptkbp:bfsLayer
|
6
|