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Expendable medium-lift launch vehicle
H-IIA (H-2A) is a retired Japanese expendable launch system that was developed and operated by Mitsubishi Heavy Industries (MHI) in collaboration with
H-IIA
is a list of launches made by JAXA using H-II series of rockets which also includes the H-IIA and H-IIB. The H-II series was Japan's first medium-lift
List_of_H-II_series_launches
List of launches by Japan's Aerospace Exploration Agency
2013. Space Launch Report: H-IIA/B Data Sheet, Retrieved 20 February 2019 "Launch Result of the IBUKI (GOSAT) by H-IIA Launch Vehicle No. 15". MHI and
List_of_JAXA_launches
Expendable launch system
its predecessor, the H-IIA. Its performance to low Earth orbit (LEO) was sufficient to carry the 16,500 kg (36,400 lb) HTV. The H-IIB made its debut in
H-IIB
Japanese rocket
later use the H-IIA's technologies (the rocket itself is the successor to the H-II) to create the Delta III, albeit short lived). Although the H-I did have
H-II
H-II Kuaizhou Long March PSLV R-7 Vega Others Antares 230+ Ariane 5 Atlas V Electron Falcon 9 new Falcon 9 reused Falcon Heavy H-IIA
2020_in_spaceflight
H-IIA Launch Vehicle No. 15". MHI and JAXA. January 23, 2009. "H-IIA F16". Sorae. Archived from the original on 2012-02-18. "Launch Day of the H-IIA Launch
List of Yoshinobu Launch Complex launches
List_of_Yoshinobu_Launch_Complex_launches
Japanese launch complex
complex was initially developed for the H-II launch vehicle and has since supported launches of the H-IIA, H-IIB, and H3 rockets. The complex consists
Yoshinobu_Launch_Complex
Japan's national air and space agency
operations of the H-IIA liquid-fueled launch vehicle, the M-V solid-fuel launch vehicle, and several observation rockets from each agency. The H-IIA is a launch
JAXA
Launch services joint venture between Arianespace and Mitsubishi Heavy Industries
customer's discretion. The LSA offered this service for the Ariane 5 and H-IIA expendable launch systems; it previously offered the Zenit-3SL as well.
Launch_Services_Alliance
Launch system that uses a single use launch vehicle
all other H-IIA launches were successful, and as of June 2025, the H-IIA had successfully launched 48 of its 49 launches. JAXA ended H-IIA operations
Expendable_launch_system
Guided-missile destroyer class in the Japanese Maritime Self-Defense Forces
larger than aboard the American counterparts, Arleigh Burke-class Flight IIA. One of the most obvious changes is an additional hangar to carry one SH-60K
Atago-class_destroyer
Japanese medium-lift launch vehicle
Industries (MHI). A hydrolox-fuelled rocket, it is the successor to the H-IIA and H-IIB launch vehicles. The H3 uses the LE-9 main engine, which was designed
H3_(rocket)
Family of Japanese solid rocket boosters
boosters developed and manufactured by IHI Corporation for use on the H-IIA, H-IIB, Epsilon, H3, and Epsilon S launch vehicles. The earlier versions,
SRB-A
Canadian satellite communications company
Services (formerly H-IIA Launch Services) launched Telstar 12 VANTAGE for Telesat in November 2015 on a H2A204 variant of the H-IIA rocket, and it commenced
Telesat
Rocket-launch complex in Japan
LA-Y1 H-IIA Flight 13 (Kaguya) launch from LA-Y1, 2007 H-IIA Flight 23 (GPM) rollout to LA-Y1, 2014 H-IIA Flight 23 (GPM) at LA-Y1, 2014 H-IIA rocket
Tanegashima_Space_Center
Japanese anti-ship and land-attack missile
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Type 12 surface-to-ship missile
Type_12_surface-to-ship_missile
Japanese multinational corporation
renamed MHI RJ Aviation Group. Space launch vehicles: H-I (with license from McDonnell-Douglas) H-II H-IIA H-IIB H3 N-I (with license from McDonnell-Douglas)
Mitsubishi_Heavy_Industries
Guided-missile destroyer class in the Japanese Maritime Self-Defense Forces
Ishikawajima-Harima LM2500 gas turbines giving them a top speed of 30 knots (56 km/h; 35 mph). Starboard beam view of the JS Kirishima All four Kongo-class destroyers
Kongō-class_destroyer
Japanese regional navigation satellite system
2009. "Launch Result of the First Quasi-Zenith Satellite "MICHIBIKI" by H-IIA Launch Vehicle No. 18". JAXA. 11 September 2010. Archived from the original
Quasi-Zenith_Satellite_System
Japanese main battle tank
10 tank boasts high mobility, including a backward movement speed of 70 km/h (43 mph). The engine was to power the Turkish Altay tank. However, negotiations
Type_10
Japanese hydrolox staged combustion rocket engine
Japanese) Japanese Wikipedia LE-7A page (in Japanese) H-IIA Rocket Engine Development Overview of the H-IIA Launch Vehicle Includes H-IIA-F6 failure analysis
LE-7
Japanese weather satellite
DS-2000 bus. Himawari 9 was launched on 2 November 2016, 06:20:00 UTC, atop a H-IIA rocket flying from the Yoshinobu Launch Complex Pad 1 at the Tanegashima
Himawari_9
Class of the Japan Maritime Self-Defense Force
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Akizuki-class destroyer (2010)
Akizuki-class_destroyer_(2010)
Japanese liquid-fuelled carrier rocket
N-II Delta rocket H-II H-IIA PGM-17 Thor Comparison of orbital launchers families Comparison of orbital launch systems Japan's H–1 and H–2 rockets, Air &
H-I
Island within Ōsumi Islands
Technology Museum The H-IIA F11 launch vehicle lifting off from Tanegashima Space Center A Mitsubishi Heavy Industries (MHI) H-IIA rocket at TSC The Tanegashima
Tanegashima
Main battle tank
The maximum quoted road speed of the Type 74 is 53 km/h; however, speeds of at least 60 km/h have been achieved. Instead of composite armour (as used
Type_74_tank
Japanese infantry fighting vehicle
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Mitsubishi_Type_89_IFV
Topics referred to by the same term
submarines H-II, a family of Japanese liquid-fueled rockets H-IIA H-IIB H-II Transfer Vehicle, a Japan Aerospace Exploration Agency uncrewed spacecraft H II region
HII
Canadian commercial communications satellite
dedicated commercial payload of the Japanese H-IIA launch vehicle. Graham, William (2015-11-23). "Japanese H-IIA successfully lofts Telstar 12V". NASAspaceflight
Telstar_12V
Main battle tank
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Type_61_(tank)
Type of rocket engine which uses liquid fuel stored at very low temperatures
almost the highest specific impulse." "Le-7A｜エンジン｜H-Iiaロケット｜ロケット｜Jaxa 宇宙輸送技術部門". "Le-5B｜エンジン｜H-Iiaロケット｜ロケット｜Jaxa 宇宙輸送技術部門". "Le-9｜エンジン｜H3ロケット｜ロケット｜Jaxa
Cryogenic_rocket_engine
Japanese truck-launched anti-ship missile
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Type 88 surface-to-ship missile
Type_88_surface-to-ship_missile
launch vehicle, planned to cost less than half that of its predecessor H-IIA; the maiden launch of NASA's Space Launch System (SLS) super heavy-lift
2021_in_spaceflight
Anti-ship cruise missiles
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Type_91_air-to-ship_missile
Joint venture between Mitsubishi Heavy Industries and Caterpillar Inc.
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Mitsubishi Caterpillar Forklifts
Mitsubishi_Caterpillar_Forklifts
JMSDF submarine
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Sōryū-class_submarine
Space program of Japan
about the same time as the H-II launcher was downscaled to the smaller H-IIA. The HOPE-X was to be launched on the H-IIA vehicle. The project was cancelled
Japanese_space_program
Japanese weather satellite
(Himawari 7) which was launched in 2006. Himawari 8 was launched atop a H-IIA rocket flying from the Yoshinobu Launch Complex Pad 1 at the Tanegashima
Himawari_8
Japanese main battle tank
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Type_90_tank
August 15, 2017. Chassefière, E.; Korablev, O.; Imamura, T.; Baines, K. H.; Wilson, C. F.; Titov, D. V.; Aplin, K. L.; Balint, T.; Blamont, J. E. (1
List_of_missions_to_Venus
Japanese spy satellites
the cabinet. All Information Gathering Satellites have been launched by H-IIA rockets from the Tanegashima Space Center. On 28 March 2003, presumably
Information Gathering Satellite
Information_Gathering_Satellite
Space exploration probe mission to Mars
Center in Japan with a Japanese rocket, the Mitsubishi Heavy Industries H-IIA launch vehicle. All three arrived at Mars in February 2021. The Emirates
Emirates_Mars_Mission
Japanese communications satellite
successfully deployed on 24 January 2017 using a H-IIA rocket flying in its heaviest configuration, the H-IIA 204. It is Japan's first dedicated military communication
DSN-2
Name of various communications satellites
launched Telstar 12 Vantage in November 2015 on a H2A204 variant of the H-IIA rocket, and it commenced service in December 2015. Telstar 19V was launched
Telstar
Ariane 6 Atlas V Ceres-1 Electron Falcon 9 new Falcon 9 reused H-IIA H3 GSLV LVM3 PSLV Jielong 3 Kinetica 1 Kuaizhou 1A Kuaizhou
2025_in_spaceflight
Japanese attack submarine class
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Taigei-class_submarine
Japanese ship-launched anti-ship missile
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Type_90_ship-to-ship_missile
Japanese hydrolox rocket engine used on the H3 upper stage
issued. *, tank head pressure only H-I Japanese carrier rocket H-II Japanese carrier rocket H-IIA Japanese carrier rocket H-IIB Japanese carrier rocket LE-7 –
LE-5
Japanese-American rocket stage
Development Agency of Japan, based on the second stage it developed for the H-IIA rocket. The initial versions for the Delta III were built by Mitsubishi
Delta_Cryogenic_Second_Stage
Japanese supersonic strike/attack aircraft
35.6 kN (8,000 lbf) with afterburner Performance Maximum speed: 1,700 km/h (1,100 mph, 920 kn) at 11,000 m (36,000 ft) (clean) Combat range: 556 km (345 mi
Mitsubishi_F-1
Solid-fuel orbital vehicle component
Programme, with launches from Esrange in Sweden. Certain versions of the H-IIA rockets flown by JAXA used either two or four strap-on boosters developed
Castor_(rocket_stage)
Nuclear reactor design
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Atmea
Japanese communications demonstration satellite
launch had to be put on hold. Using the H-IIA was out of question: it would have been overkill to use the H-IIA to send a 570 kilograms (1,260 lb) satellite
OICETS
Failed Japanese X-ray astronomy satellite
of 31.01°. It was launched from the Tanegashima Space Center on board an H-IIA launch vehicle. 14 minutes after launch, the satellite separated from the
Hitomi_(satellite)
Guided-missile destroyer class in the Japanese Maritime Self-Defense Forces
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Hatakaze-class_destroyer
Japansese submarine class
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Oyashio-class_submarine
Japanese nuclear reactor design
EU-APWR" (PDF). Nuclear Energy for New Europe 2008. Aeba, Y. F.; Weiss, E. H. (1999). "APWR - Mitsubishi, Japan/Westinghouse, USA". Strategic issues, technologies
Mitsubishi_APWR
H-II Long March Minotaur Mu R-7 R-36 Space Shuttle Universal Rocket Zenit Others Ariane 5 Atlas V Delta II Delta IV Delta IV Heavy H-IIA
2006_in_spaceflight
Aerospace subsidiary of Mitsubishi Heavy Industries
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Mitsubishi Aircraft Corporation
Mitsubishi_Aircraft_Corporation
JAXA small-lift rocket family
launch the Epsilon uses the existing SRB-A3, a solid rocket booster on the H-IIA rocket, as its first stage. Existing M-V upper stages will be used for the
Epsilon_(rocket)
Japan Mitsubishi, JAXA H-IIA, H-IIB Active Upper LH2 / LOX Expander, open 447 137,000 36.0 269 51.93 5 LE-7 Japan Mitsubishi, NASDA H-II Retired 1st LH2
Comparison of orbital rocket engines
Comparison_of_orbital_rocket_engines
Topics referred to by the same term
H2 H-II, a family of Japanese liquid-fueled rockets H-IIA H-IIB H-II Transfer Vehicle, a Japan Aerospace Exploration Agency uncrewed spacecraft H-2 MUPSOW
H2
Space launch vehicle
used on the N-I Comparison of orbital launchers families Delta rocket H-I H-II H-IIA N-I rocket PGM-17 Thor "JAXA | Engineering Test Satellite IV "KIKU-3"
N-II_(rocket)
Philippine microsatellite
that on October 26, 2018, the satellite would be launched to space via the H-IIA from Japan at the Tanegashima Space Center at around 13:08 and 13:20 (JST)
Diwata-2
Japanese diesel-electric submarine
On the surface, the ships were capable of 12 knots (22 km/h; 14 mph) and 20 knots (37 km/h; 23 mph) while dived. The Harushio class mounted six 533-millimetre
Harushio-class_submarine
Extreme benchmarks set off Earth by astronauts, launchers and probes
Retrieved June 22, 2023. "Japanese H-IIA Rocket Fires Into Orbit with Climate Change Satellite & Super-Low Altitude Testbed – H-IIA – GCOM-C1". Spaceflight101
List_of_spaceflight_records
Electron Falcon 9 new Falcon 9 reused Falcon Heavy GSLV Mk II H-IIA H-IIB Long March 2 Long March 3 Long March 4 Long March 11 PSLV
2018_in_spaceflight
Japanese Earth observation satellite
organizations. GOSAT was launched along with seven other piggyback probes using the H-IIA, Japan's primary large-scale expendable launch system, at 3:54 am on 23
Greenhouse Gases Observing Satellite
Greenhouse_Gases_Observing_Satellite
Consortium of 3 Japanese companies
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Japanese Aero Engine Corporation
Japanese_Aero_Engine_Corporation
Japanese experimental spaceplane
next year the H-II project was cancelled outright, proceeding with the simplified and lighter H-IIA alone. Hughes pulled out of the H-IIA project at about
HOPE-X
Geostationary meteorological satellite
4 Dec 2015 H-IIA (F7) Tanegashima MTSAT-2 (Himawari 7) 18 Feb 2006 10 Mar 2017 H-IIA (F9) Tanegashima Himawari 8 7 Oct 2014 Stand-by H-IIA (F25) Tanegashima
Himawari_(satellites)
Electron Falcon H-series ILV Kinetica Kuaizhou Long March R-7 Others Ceres-1 Electron Falcon 9 new Falcon 9 reused Falcon Heavy H-IIA H3 GSLV
2024_in_spaceflight
Space launch vehicle
Development Agency of Japan based on the second stage it developed for the H-IIA rocket and built by Mitsubishi Heavy Industries. Contraves built the fairing
Delta_III
Japanese launch complex
test involving an SRB-A solid rocket booster, which is utilized on the H-IIA launch vehicle. The Osaki Launch Complex was deactivated in the mid-1990s
Osaki_Launch_Complex
Heavyweight ASuW torpedo
knots (102 km/h) maximum possibly 70 knots (130 km/h) Range: 27 nmi (50 km) at 40 knots (74 km/h), 21 nmi (39 km) at 55 knots (102 km/h). Operating depth:
Type_89_torpedo
Change in velocity per amount of fuel
inversely proportional to specific impulse and has units of g/(kN·s) or lb/(lbf·h). Specific fuel consumption is used extensively for describing the performance
Specific_impulse
Category of space launch vehicle
family were introduced in the 1970s. Japan launched the H-I in 1986 before developing the H-II and H3. India introduced the PSLV in 1993 and LVM3 in
Medium-lift_launch_vehicle
Japanese rugby union club, based in Sagamihara
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Mitsubishi Sagamihara DynaBoars
Mitsubishi_Sagamihara_DynaBoars
Japanese writer (born 1978)
since 2007. On 2 November 2016 his artwork was carried into space by the H-IIA rocket carrying the Himawari-9 weather satellite as part of an outreach
Chūya_Koyama
Delta H-II Long March R-7 R-14 Space Shuttle Titan UR Others Ariane 4 Ariane 5 Atlas II Atlas III Atlas V Delta II Delta IV H-IIA Long
2002_in_spaceflight
CISC microprocessor
H-IIA carrier rockets, in satellites such as the Akatsuki (Venus Climate Orbiter), and the Kibo International Space Station (ISS) module. The H-IIA launch
NEC_V60
Falcon H-series Kuaizhou Long March PSLV R-7 Others Ceres-1 Chŏllima 1 Electron Falcon 9 new Falcon 9 reused Falcon Heavy H-IIA H3 Kuaizhou-1A
2023_in_spaceflight
Japanese orbiter mission to Venus (2010–2024)
tasked with studying the atmosphere of Venus. It was launched aboard an H-IIA 202 rocket on 20 May 2010, but failed to enter orbit around Venus on 6 December
Akatsuki_(spacecraft)
US Navy guided-missile destroyer class
Flight IIA ship USS Mustin without TACTAS and no Harpoon launchers, but with helicopter hangars and new exhaust stacks design Flight III ship USS Jack H. Lucas
Arleigh_Burke-class_destroyer
First interplanetary solar sail spacecraft
experimental spacecraft. The spacecraft was launched on 20 May 2010, aboard an H-IIA rocket, together with the Akatsuki (Venus Climate Orbiter) probe and four
IKAROS
Aircraft engine that produces thrust by emitting a jet of gas
cycle diagram. The engine efficiency, or thermal efficiency, known as η t h {\displaystyle \eta _{th}} . is dependent on the Thermodynamic cycle parameters
Jet_engine
Japanese low-floor light-rail vehicle
frequency) motor capable of regenerative braking, maximum service speeds of 80 km/h (50 mph), and LRVs for both 1,435 mm (4 ft 8+1⁄2 in) standard gauge and 1
Green_Mover_Max
Geostationary communications satellite bus
is compatible with Ariane 5, Proton-M, Zenit-3SL, Atlas V, Falcon 9 and H-IIA. According to Moog-ISP, the DS2000 platform uses its bipropellant thrusters
DS2000
Delta Falcon H-II Long March Minotaur PSLV R-7 UR Vega Others Ariane 5 Atlas V Delta II Delta IV Falcon 9 new Falcon 9 reused H-IIA Long March
2017_in_spaceflight
Japanese solid-fuel rocket designed to launch scientific satellites
capability. The development aim is to reduce costs, primarily by using the H-IIA solid rocket booster as the first stage and through shorter launch preparation
M-V
Satellite (STARS) mission launched 23 January 2009 as a secondary payload on a H-IIA launch. After launch, the satellite was named KUKAI, and consisted of two
List_of_CubeSats
Japanese interplanetary spacecraft
on 20 May 2010. It was being launched as a secondary payload aboard an H-IIA 202 rocket, with the primary payload being the Akatsuki spacecraft bound
Shin'en_(spacecraft)
Transportation equipment brand
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Mitsubishi_Logisnext
Ship class
KDX-IIA is an Aegis Combat System armed variant of the KDX-II, Chungmugong Yi Sun-sin-class destroyer of the Republic of Korea Navy (ROKN). As of 2011
KDX-IIA
Circular orbit above Earth's Equator and following the direction of Earth's rotation
William (October 6, 2014). "Japan lofts Himawari 8 weather satellite via H-IIA rocket". NASASpaceFlight.com. "China plans to launch additional nine Fengyun
Geostationary_orbit
astronautix.com, H-2 Archived 2008-07-06 at the Wayback Machine Krebs, Gunter. "H-2". Gunter's Space Page. Retrieved 1 August 2011. "H-IIA Launch Vehicle"
Comparison of retired orbital launch systems
Comparison_of_retired_orbital_launch_systems
Aircraft manufacturer in Japan
Nana-yon Type 89 IFV Type 90 tank Type 10 Launch vehicles N-I N-II H-I H-II H-IIA H-IIB H3 Missiles Type 88 Type 89 Type 90 Type 91 Ships Akizuki class Atago
Nihon Aircraft Manufacturing Corporation
Nihon_Aircraft_Manufacturing_Corporation
Delta H-II Long March PSLV R-7 R-14 R-36 Space Shuttle Universal Rocket Zenit Others Ariane 5 Atlas V Delta II Delta IV Delta IV Heavy H-IIA
2007_in_spaceflight
Japan licensed built variant of McDonnell Douglas F-15
afterburner Performance Maximum speed: 2,650 km/h (1,650 mph, 1,430 kn) / M2.5+ at high altitude 1,450 km/h (900 mph; 780 kn) / M1.2 at low altitude Service
Mitsubishi_F-15J
H IIA
H IIA
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H IIA
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H IIA
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H IIA