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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:configuration
|
Epsilon 1, Epsilon 2, Epsilon 3
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:debut
|
gptkb:2013
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|
gptkbp:design_purpose
|
small satellite launches
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|
gptkbp:development
|
gptkb:2007
|
|
gptkbp:development_cost
|
$100 million
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:engine_type
|
solid rocket motor
|
|
gptkbp:first_flight
|
TBD
September 14, 2013
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:height
|
26 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Epsilon rocket
|
|
gptkbp:launch_date
|
approximately once a year
|
|
gptkbp:launch_platform
|
gptkb:Japan_Aerospace_Exploration_Agency
|
|
gptkbp:launch_price
|
approximately $10 million
|
|
gptkbp:launch_site
|
gptkb:Uchinoura_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Epsilon_family
|
|
gptkbp:launched
|
multiple satellites
|
|
gptkbp:manufacturer
|
gptkb:JAXA
|
|
gptkbp:notable_launches
|
H-IIA and H-IIB missions
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
gptkb:textiles
1,200 kg to LEO
|
|
gptkbp:purpose
|
gptkb:Space_Launch_System
|
|
gptkbp:reliability
|
high
|
|
gptkbp:strategic_goals
|
gptkb:0
|
|
gptkbp:success
|
gptkb:5
|
|
gptkbp:success_rate
|
100% as of 2021
100% for first three flights
|
|
gptkbp:successor
|
gptkb:Epsilon_S
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:bfsLayer
|
4
|