|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:controls
|
digital flight control system
|
|
gptkbp:design
|
10 years
|
|
gptkbp:developer
|
$100 million
|
|
gptkbp:diameter
|
2.6 meters
|
|
gptkbp:education
|
yes
|
|
gptkbp:engine
|
4
|
|
gptkbp:engineType
|
solid rocket motor
|
|
gptkbp:environmentalImpact
|
low
|
|
gptkbp:firstAwarded
|
TBD
|
|
gptkbp:firstFlight
|
September 14, 2013
completed successfully
|
|
gptkbp:firstGeneration
|
data review
|
|
gptkbp:fuelType
|
gptkb:HTPB
|
|
gptkbp:future_plans
|
ongoing
|
|
gptkbp:futurePlans
|
upgraded versions
|
|
gptkbp:height
|
26 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Epsilon rocket
|
|
gptkbp:integration
|
2 weeks
|
|
gptkbp:internationalCooperation
|
yes
|
|
gptkbp:launchDate
|
5 successful launches
|
|
gptkbp:launched
|
gptkb:JAXA
varies
$10 million
remote control
1-2 per year
pre-launch checks
dedicated launch complex
|
|
gptkbp:launchSite
|
gptkb:Uchinoura_Space_Center
|
|
gptkbp:launchVehicle
|
gptkb:Epsilon_family
|
|
gptkbp:manufacturer
|
gptkb:JAXA
gptkb:Japan
|
|
gptkbp:marketSegment
|
yes
|
|
gptkbp:mediaCoverage
|
extensive
|
|
gptkbp:missionCapabilities
|
vertical_ascent
|
|
gptkbp:notableFeature
|
H-IIA 202
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operationalStatus
|
2013
active
|
|
gptkbp:partnerships
|
various universities
|
|
gptkbp:passenger_traffic
|
scientific satellites
2.5 meters in diameter
|
|
gptkbp:payloadCapacity
|
Low Earth Orbit
1,200 kg to LEO
|
|
gptkbp:propulsion
|
300 kN
50:1
|
|
gptkbp:provides
|
inertial navigation system
|
|
gptkbp:publicAccess
|
high
|
|
gptkbp:purpose
|
satellite launch
|
|
gptkbp:reliability
|
no
high
|
|
gptkbp:researchInterest
|
Earth_observation
|
|
gptkbp:safetyFeatures
|
excellent
|
|
gptkbp:setting
|
Epsilon_1,_Epsilon_2,_Epsilon_3
|
|
gptkbp:skills
|
0
|
|
gptkbp:succeededBy
|
5
100% as of 2021
|
|
gptkbp:transportation
|
road transport
|