|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:capacity
|
4,000 kg
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:events
|
successful
|
|
gptkbp:first_flight
|
217
2021-03-30
2004-08-29
2001-08-29
|
|
gptkbp:gps
|
gptkb:Tanegashima
|
|
gptkbp:home_ground
|
gptkb:Kagoshima
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 217
|
|
gptkbp:launch_date
|
completed
2005-02-20
2019-01-18
10:43 UTC
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
gptkb:H-IIA_202
2000 kg
|
|
gptkbp:launched
|
gptkb:musical
gptkb:standard
217
completed
two-stage
open
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
gptkb:satellite
completed
Sun-synchronous orbit
Satellite launch
DSN-1
Geostationary transfer orbit
|
|
gptkbp:mission_duration
|
gptkb:CEO
5 years
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B_engine
LE-7 A engine
|
|
gptkbp:operator
|
gptkb:JAXA
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:orbital_inclination
|
98.2 degrees
|
|
gptkbp:outcome
|
100%
|
|
gptkbp:purpose
|
gptkb:spacecraft
|
|
gptkbp:restoration
|
not applicable
|
|
gptkbp:seating_capacity
|
gptkb:Akasaki
gptkb:DAICHI-2
gptkb:satellite
600 kg
successful
4,000 kg to geostationary transfer orbit
|
|
gptkbp:succeeded_by
|
gptkb:theorem
100%
95%
|