Statements (126)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
gptkb:rocket |
| gptkbp:bfsLayer |
3
|
| gptkbp:bfsParent |
gptkb:rocket
|
| gptkbp:collaborations |
NASA, ESA.
|
| gptkbp:controls |
Digital control system
|
| gptkbp:debut_year |
Part of the H-IIA program
over 30 launches since introduction. |
| gptkbp:design |
satellite launch.
|
| gptkbp:developer |
estimated at $1 billion.
|
| gptkbp:diameter |
4 meters
|
| gptkbp:durability |
not reusable.
|
| gptkbp:elevation |
4 meters.
53 meters. |
| gptkbp:engine |
1 main engine.
single engine. |
| gptkbp:engine_type |
gptkb:LE-7_A
liquid-fueled. |
| gptkbp:events |
100%
over 95% successful |
| gptkbp:first_flight |
gptkb:2001
2014-02-22 2004-08-29 |
| gptkbp:fuel_type |
Liquid hydrogen and kerosene
|
| gptkbp:guidance_system |
Inertial guidance system
inertial navigation. |
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 204
|
| gptkbp:launch_date |
2021-03-30
2014-12-03 Approx. 30 minutes approximately 2-3 per year 2-3. 2004-08-29 2021-03-30. |
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
gptkb:JAXA Japan. Japan Aerospace Exploration Agency (JAXA Mitsubishi Heavy Industries. Tanegashima Space Center. Tanegashima. |
| gptkbp:launch_vehicle |
gptkb:H-IIA
approximately 300 tons ongoing. active. 200,000 kg 2. international partnerships. high reliability. planned upgrades. 204. 53m height, 4m diameter. JAXA. Launch Complex 1. advanced guidance systems. commercial and scientific missions. expendable launch vehicle. high payload capacity. medium-lift. operational since 2004. satellite deployment. significant in Japanese space history. solid rocket boosters. two-stage. |
| gptkbp:launched |
gptkb:television_series
gptkb:Akasaki_satellite multiple over 40 several months. varies by mission. Standard configuration over 30. two solid rocket boosters. |
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:market |
approximately $90 million.
|
| gptkbp:mission |
gptkb:H-IIA_205
successful satellite deployment Satellite launch high. geostationary transfer orbit DSN-1 H-IIA 203 commercial, scientific. |
| gptkbp:mission_duration |
approximately 30 minutes
|
| gptkbp:notable_achievement |
successful ISS resupply missions.
|
| gptkbp:notable_album |
H-IIA 204 launched Akasaki satellite
H-IIA 204 launched Akasaki satellite. |
| gptkbp:number_of_stages |
gptkb:LE-5_B_engine
2 LE-7 A engine |
| gptkbp:operational_status |
Retired
active 2004. |
| gptkbp:operator |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:orbital_inclination |
20 degrees
geostationary. |
| gptkbp:primary_user |
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
| gptkbp:propulsion |
1,000 k N
1,000 k N. |
| gptkbp:reliability |
gptkb:High
high |
| gptkbp:safety_record |
excellent.
|
| gptkbp:seating_capacity |
gptkb:H-IIA_202
gptkb:satellite 4 meters 4,000 kg 4 meters in diameter 4,000 kg to geostationary transfer orbit Multiple payloads deployed 4 meters. H-II Transfer Vehicle. done at Tanegashima. scientific, commercial. up to 4,000 kg. various orbits. various satellites. |
| gptkbp:setting |
204
|
| gptkbp:strategic_importance |
gptkb:0
|
| gptkbp:succeeded_by |
gptkb:10
gptkb:theorem over 90% multiple satellite deployments. |
| gptkbp:upgrades |
upgraded engines.
|