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le manufacturer mitsubishi heavy industries country of origin japan cost per launch us 90 million 1 size height 53 m 174 ft diameter 4 m 13 ft mass 285 000 445 000 kg 628 000 981 000 lb stages 2 capacity payload to leo mass 10 000 15 000 kg 22 000 33 000 lb payload to gto mass 4 100 6 000 kg 9 000 13 200 lb associated rockets family h ii family based on h ii derivative work h iib h3 launch history status retired launch sites tanegashima la y1 total launches 50 202 35 204 5 2022 3 2024 7 success es 49 202 35 204 5 2022 3 2024 6 first flight 202 29 august 2001 204 18 december 2006 2022 26 february 2005 2024 4 february 2002 last flight 202 28 june 2025 204 22 december 2021 2022 14 september 2007 2024 23 february 2008 carries passengers or cargo selene ibuki akatsuki hayabusa 2 emirates mars mission boosters srb a no boosters 2 4 height 15 1 m 50 ft diameter 2 5 m 8 ft 2 in maximum thrust 2 260 kn 510 000 lb f total thrust 4 520 9 040 kn 1 020 000 2 030 000 lb f specific impulse 280 s 2 7 km s burn time 120 seconds propellant htpb boosters 2022 2024 castor 4a xl no boosters 2 4 height 12 m 38 ft diameter 1 02 m 40 1 in 2 gross mass 14 983 kg 33 031 lb propellant mass 13 112 kg 28 906 lb maximum thrust 765 kn 172 060 lbf total thrust 1 531 3 061 kn 344 120 688 240 lbf specific impulse 282 6 s 2 771 km s burn time 58 seconds propellant htpb al first stage height 37 2 m 122 ft diameter 4 m 13 ft powered by 1 le 7a maximum thrust 1 098 kn 247 000 lb f specific impulse 440 s 4 3 km s burn time 390 seconds propellant lh 2 lox second stage height 9 2 m 30 ft diameter 4 m 13 ft powered by 1 le 5b maximum thrust 137 kn 31 000 lb f specific impulse 447 s 4 38 km s burn time 534 seconds propellant lh 2 lox edit on wikidata h iia h 2a is a retired japanese expendable launch system that was developed and operated by mitsubishi heavy industries mhi in collaboration with jaxa it was primarily used to launch satellites into geostationary orbit interplanetary probes and earth observation missions notable payloads launched by the h iia include akatsuki a venus climate orbiter and the emirates mars mission which was launched toward mars in july 2020 all launches were conducted from the tanegashima space center the h iia made its maiden flight on 29 august 2001 and flew a total of 50 times before its retirement on 28 june 2025 it achieved 49 successful launches including a streak of 44 consecutive missions from 2003 to 2025 management and production responsibility was transferred from jaxa to mhi on 1 april 2007 with flight 13 carrying the selene lunar orbiter being the first mission under private operation 3 the h iia was derived from the earlier h ii launch vehicle and featured significant design changes aimed at improving reliability and reducing cost several variants were developed with the final configuration designated h2a 202 retired in 2025 a derivative design the h iib was introduced in 2009 and retired in 2020 the h ii series of launch vehicles have been succeeded by the h3 rocket which conducted its first flight in march 2023 vehicle description and variants edit h iia rocket variants the h iia had two stage core powered by liquid hydrogen and liquid oxygen and various configurations of boosters to provide additional thrust based on mission requirements the base and final active configuration h2a 202 used two srb a type solid rocket boosters launch performance could be enhanced by adding up to two additional srb as for a total of four boosters or by adding up to four castor 4axl solid strap on boosters ssbs for a total of six boosters h iia configurations were designated by a three or four digit code following the prefix h2a 4 the first digit indicates the number of core stages always 2 the second digit indicates the number of liquid rocket boosters which were planned but never developed always 0 the third digit indicates the number of srb a solid rocket boosters 2 or 4 the optional fourth digit indicates the number of castor 4axl strap on boosters 2 or 4 status retired never flown designation mass t lb payload to gto t lb boosters h2a 202 285 628 000 4 1 9 000 2 srb a srb h2a 2022 5 316 697 000 4 5 9 900 2 srb a srb 2 castor 4axl ssb h2a 2024 347 765 000 5 11 000 2 srb a srb 4 castor 4axl ssb h2a 204 445 981 000 6 13 000 4 srb a srb h2a 212 403 888 000 7 5 17 000 2 srb a srb 1 lrb 6 7 h2a 222 520 1 150 000 9 5 21 000 2 srb a srb 2 lrbs 6 launch history edit main article list of h ii series launches the first h iia was successfully launched on 29 august 2001 followed by a string of successes the sixth launch on 29 november 2003 intended to launch two igs reconnaissance satellites failed jaxa announced that launches would resume in 2005 and the first successful flight took place on 26 february 2005 with the launch of mtsat 1r the first launch for a mission beyond earth orbit was on 14 september 2007 for the selene moon mission the first foreign payload on the h iia was the australian fedsat 1 in 2002 as of march 2015 27 out of 28 launches were successful a rocket with increased launch capabilities h iib is a derivative of the h iia family h iib uses two le 7a engines in its first stage as opposed to one in h iia the first h iib was successfully launched on 10 september 2009 for the 29th flight on 24 november 2015 an h iia with an upgraded second stage 8 launched the telstar 12v satellite the first commercial primary payload for a japanese launch vehicle 9 flight date utc type payload s outcome tf1 29 august 2001 07 00 00 h2a 202 vep 2 lre success tf2 4 february 2002 02 45 00 h2a 2024 vep 3 mds 1 tsubasa dash success f3 10 september 2002 08 20 00 h2a 2024 users drts kodama success f4 14 december 2002 01 31 00 h2a 202 adeos 2 midori 2 weos kanta kun fedsat 1 micro labsat 1 success f5 28 march 2003 01 27 00 h2a 2024 igs optical 1 igs radar 1 success f6 29 november 2003 04 33 00 h2a 2024 igs optical igs radar failure a hot gas leak from srb a motor destroyed its separation system and the booster did not separate as planned the weight of the spent motor prevented the vehicle from achieving its planned speed and height and it was destroyed via a ground command about 10 minutes into the flight 10 f7 26 february 2005 09 25 00 h2a 2022 mtsat 1r himawari 6 success f8 24 january 2006 01 33 00 h2a 2022 alos daichi success f9 18 february 2006 06 27 00 h2a 2024 mtsat 2 himawari 7 success f10 11 september 2006 04 35 00 h2a 202 igs optical 2 success f11 18 december 2006 06 32 00 h2a 204 ets viii kiku 8 success f12 24 february 2007 04 41 00 h2a 2024 igs radar 2 igs optical 3v success f13 14 september 2007 01 31 01 h2a 2022 selene kaguya success f14 23 february 2008 08 55 00 h2a 2024 winds kizuna success f15 23 january 2009 03 54 00 h2a 202 gosat ibuki sds 1 stars kūkai kks 1 kiseki prism hitomi sohla 1 maido 1 sorunsat 1 kagayaki sprite sat raijin success 11 f16 28 november 2009 01 21 00 12 h2a 202 igs optical 3 success f17 20 may 2010 21 58 22 13 14 15 h2a 202 16 planet c akatsuki ikaros unitec 1 shin en waseda sat2 k sat hayato negai success f18 11 september 2010 11 17 00 17 h2a 202 qzs 1 michibiki success f19 23 september 2011 04 36 50 18 h2a 202 igs optical 4 success f20 12 december 2011 01 21 00 19 h2a 202 igs radar 3 success f21 17 may 2012 16 39 00 h2a 202 20 gcom w1 shizuku kompsat 3 arirang 3 sds 4 horyu 2 success f22 27 january 2013 04 40 00 h2a 202 igs radar 4 igs optical 5v success f23 27 february 2014 18 37 00 h2a 202 gpm core sindaisat ginrei stars ii gennai teikyosat 3 itf 1 yui opusat cosmoz invader ksat2 success f24 24 may 2014 03 05 14 h2a 202 alos 2 daichi 2 rising 2 uniform 1 socrates sprout success f25 7 october 2014 05 16 00 h2a 202 himawari 8 success f26 3 december 2014 04 22 04 h2a 202 hayabusa2 shin en 2 artsat2 despatch procyon success f27 1 february 2015 01 21 00 h2a 202 igs radar spare success f28 26 march 2015 01 21 00 h2a 202 igs optical 5 success f29 24 november 2015 06 50 00 h2a 204 telstar 12 vantage success f30 17 february 2016 08 45 00 h2a 202 astro h hitomi chubusat 2 kinshachi 2 chubusat 3 kinshachi 3 horyu 4 success the hitomi telescope broke apart 37 days after launch 21 f31 2 november 2016 06 20 00 h2a 202 himawari 9 success f32 24 january 2017 07 44 00 h2a 204 dsn 2 kirameki 2 success f33 17 march 2017 01 20 00 h2a 202 igs radar 5 success f34 1 june 2017 00 17 46 h2a 202 qzs 2 michibiki 2 success f35 19 august 2017 05 29 00 h2a 204 qzs 3 michibiki 3 success f36 9 october 2017 22 01 37 h2a 202 qzs 4 michibiki 4 success f37 23 december 2017 01 26 22 h2a 202 gcom c shikisai slats tsubame success f38 27 february 2018 04 34 00 h2a 202 igs optical 6 success f39 12 june 2018 04 20 00 h2a 202 igs radar 6 success f40 29 october 2018 04 08 00 h2a 202 gosat 2 ibuki 2 khalifasat diwata 2 b tenkōh stars ao aoi autcube2 gamacube success f41 9 february 2020 01 34 00 h2a 202 igs optical 7 success f42 19 july 2020 21 58 14 h2a 202 emirates mars mission hope success f43 29 november 2020 07 25 00 h2a 202 jdrs lucas success f44 26 october 2021 02 19 37 h2a 202 qzs 1r success f45 22 december 2021 15 32 00 h2a 204 inmarsat 6 f1 success f46 26 january 2023 01 50 21 h2a 202 igs radar 7 success f47 6 september 2023 23 42 11 h2a 202 xrism slim success f48 12 january 2024 04 44 26 h2a 202 igs optical 8 success f49 26 september 2024 05 24 20 h2a 202 igs radar 8 success f50 28 june 2025 16 33 03 h2a 202 gosat gw success final flight of h iia and h ii family as a whole see also edit spaceflight portal comparison of orbital launchers families comparison of orbital launch systems comparison of retired orbital launch systems references edit notes surplus missile motors sale price drives potential effects on dod and commercial launch providers government accountability office 16 august 2017 retrieved 8 september 2024 propulsion products catalog pdf northrop grumman mitsubishi and arianespace combine commercial satellite launch services satnews archived from the original on 8 february 2012 h iia launch vehicle pdf jaxa p 2 archived from the original pdf on 28 february 2008 retrieved 15 september 2007 三菱重工 h2a 2機種に半減 民営化でコスト減 mitsubishi heavy industries cuts h2a aircraft production by half to two models privatization cuts costs nikkei archived from the original on 5 january 2007 1 2 japan reenters rocket race with new improved h2a space daily 20 august 2001 retrieved 29 june 2025 krebs gunter d h 2a gunter s space page retrieved 29 june 2025 launch result of telstar 12 vantage by h iia launch vehicle no 29 jaxa 24 november 2015 retrieved 30 november 2015 graham william 23 november 2015 japanese h iia successfully lofts telstar 12v nasaspaceflight retrieved 30 november 2015 launch result of igs 2 h iia f6 jaxa 29 november 2003 archived from the original on 25 september 2011 retrieved 19 june 2013 launch result of the ibuki gosat by h iia launch vehicle no 15 mhi and jaxa 23 january 2009 archived from the original on 21 june 2013 retrieved 24 january 2009 h iia f16 sorae archived from the original on 18 february 2012 launch day of the h iia launch vehicle no 17 jaxa 3 march 2010 archived from the original on 3 june 2013 retrieved 8 march 2010 overview of secondary payloads jaxa tariq malik 18 may 2010 new venus probe to launch thursday from japan after space com retrieved 20 may 2010 chris bergin 17 may 2010 jaxa launch h iia carrying akatsuki and ikaros scrubbed nasaspaceflight retrieved 17 may 2010 new launch day of the first quasi zenith satellite michibiki by h iia launch vehicle no 18 jaxa chris bergin 23 september 2011 japanese h 2a launches with new igs military satellite nasaspaceflight chris bergin 11 december 2011 japanese h 2a lofts igs radar 3 satellite into orbit nasaspaceflight launch overview h iia launch services flight no 21 mitsubishi heavy industries archived from the original on 15 october 2017 retrieved 15 april 2012 clark stephen 18 april 2016 attitude control failures led to break up of japanese astronomy satellite spaceflight now retrieved 21 april 2016 sources japan prepares for crucial rocket launch space com retrieved 16 february 2005 h iia expendable launch vehicle spaceandtech archived from the original on 4 february 2012 retrieved 16 february 2005 external links edit wikimedia commons has media related to h iia h iia archived 12 october 2017 at the wayback machine mitsubishi heavy industries jaxa h iia english page v t e mitsubishi heavy industries mitsubishi subsidiaries mitsubishi aircraft corporation 90 mitsubishi logisnext mitsubishi fbr systems mitsubishi power systems europe primetals joint ventures current dubai metro 25 japanese aero engine corporation launch services alliance mitsubishi caterpillar forklifts defunct atmea nihon aircraft manufacturing corporation products aircraft f 1 f 2 f 15j h 60 mh2000 mitsubishi spacejet t 2 x 2 armored vehicles type 61 type 74 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 class hatakaze class kongō class takanami class submarines harushio class oyashio class sōryū class taigei class other crystal mover and urbanismo green mover max meister mitsubishi apwr wakamaru people kazuo tsukuda other mitsubishi sagamihara dynaboars products currently in development shown in italics category v t e orbital launch systems list of orbital launch systems comparison of orbital launch systems current angara 1 2 a5 ariane 6 atlas v ceres 1 1s 2 chollima 1 electron eris falcon 9 block 5 falcon heavy firefly alpha gravity 1 gslv h3 hanbit nano hyperbola 1 jielong 1 3 kairos kaituozhe 2 kinetica 1 2 kuaizhou 1 1a 11 long march 2c 2d 2f 3a 3b e 3c 4b 4c 5 5b 6 6a 6c 7 7a 8 10b 11 11h 12 12a 12b lvm3 minotaur i iv v c new glenn nuri os m1 pallas 1 proton m pslv qaem 100 qased shavit 2 simorgh sls block 1 soyuz 2 2 1a sta 2 1b stb soyuz 5 spectrum sslv tianlong 2 3 unha vega c vikram 1 vulcan centaur zhuque 2e 3 in development antares 330 bloostar blue whale 1 cyclone 4m deca eclipse epsilon s gravity 2 hyperbola 2 kinetica 2h 3 kslv iii kuaizhou 21 31 long march 9 10 10a maia miura 5 neutron new line 1 nglv nova os m 2 4 rfa one sls block 1b block 2 soyuz 7 starship terran r vikram 2 vlm vega e zero zuljanah retired antares 110 120 130 230 230 ariane 1 2 3 4 5 aslv athena i ii atlas b d e f g h i ii iii lv 3b slv 3 able agena centaur black arrow conestoga delta a b c d e g j l m n 0100 1000 2000 3000 4000 5000 ii iii iv iv heavy diamant dnepr energia epsilon europa i ii falcon 1 falcon 9 v1 0 v1 1 v1 2 full thrust feng bao 1 gslv mk i h i h ii h iia h iib juno i juno ii kaituozhe 1 kosmos original 1 2 2i 3 3m lambda 4s launcherone long march 1 1d 2a 2e 3 3b 4a mu 4s 3c 3h 3s 3sii v n1 n i n ii naro 1 paektusan pegasus standard hybrid xl pilot 2 r 7 luna molniya m l polyot soyuz original fg l m u u2 2 1v soyuz vostok sputnik voskhod vostok l k 2 2m r 29 shtil volna rocket 3 rs1 safir 1 1a 1b saturn i ib v scout x 1 blue scout ii x 2 x 2m x 3 x 3m x 4 x 2b b a b 1 d 1 a 1 e 1 ...