|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:H-IIA_family
gptkb:H-IIA_series
|
|
gptkbp:debut_year
|
gptkb:2022
August 29, 2001
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine
|
gptkb:LE-7_A
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:guidance_system
|
Inertial guidance system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 2022
|
|
gptkbp:is_used_for
|
satellite launches
|
|
gptkbp:launch_date
|
annual
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:launched
|
gptkb:musical
gptkb:40
gptkb:39
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
$90 million
|
|
gptkbp:notable_album
|
H-IIA 202 for Akasaki satellite
H-IIA 202 for Akasaki-2
H-IIA 202 for Akasaki-3
H-IIA 202 for Bepi Colombo
H-IIA 202 for Epsilon-1
H-IIA 202 for GCOM-C1
H-IIA 202 for GCOM-W1
H-IIA 202 for Hayabusa2
H-IIA 202 for Himawari-9
H-IIA 202 for Kounotori-7
H-IIA 202 for Quasi-Zenith Satellite System
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:reliability
|
high
|
|
gptkbp:seating_capacity
|
10,000 kg
4,000 kg
4.0 meters
15.0 meters
|
|
gptkbp:setting
|
gptkb:H-IIA_202
H-IIA 202, H-IIA 204, H-IIA 205
|
|
gptkbp:succeeded_by
|
98%
|