1326:
1018:
1002:
1731:
27:
941:
Kakehashi, Faulty brazing in second-stage engine cooling system caused engine burn through and cable damage resulting in shutdown midway through the upper stage's second burn, leaving spacecraft in elliptical LEO instead of GTO. Spacecraft thrusters raised orbit enough to complete some communications
641:
to launch 10 satellites. The successive failure of flight 5 in 1998 and flight 8 in the following year brought an end to the H-II series and the contract with Hughes. To investigate the cause of the failure and to direct resources into the H-IIA, NASDA cancelled flight 7 (which was to be launched
621:
In 1994, NASDA succeeded in launching the first H-II rocket, and succeeded in five launches by 1997. However, each launch cost 19 billion yen (US$ 190 million), too expensive compared to international competitors like
982:
Cavitation in the first stage hydrogen turbopump impeller caused an impeller blade to fracture, resulting in loss of fuel and rapid shutdown of the engine at T+239 s. The vehicle impacted the ocean 380 km NW of
601:
Development of the LE-7 engine which started in 1984 was not without hardships, and a worker died in an accidental explosion. The first engine was completed in 1994, two years behind the original schedule. The
3635:
This
Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
630:'s changes to the exchange rate, which was 240 yen to a dollar when the project planning started in 1982, but had changed to 100 yen a dollar by 1994.) Development of the next-generation
573:
Use design criteria which allows sufficient performance for both the main systems and subsystems. Ensure that development will be carried out properly, and safety is taken into account.
1289:
1177:"Japan Discovers It's Harder to Be a Star in Space : Aerospace: The failure of a new rocket sets back its effort to become a key player in the commercial launch business"
603:
589:
tank cylinder carried payload launch loads, while the LOX tank and engine were suspended below within the rocket's inter-stage. The second stage was powered by a single
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Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
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Prior to H-II, NASDA had to use components licensed by the United States in its rockets. In particular, crucial technologies of
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542:, the most crucial part, the first stage engine, was a licence-built version of the Thor-ELT of the US. By developing the
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618:, was established in 1990 to manage launch operations after the rockets' completion. In 1992, it had 33 employees.
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4031:‡ Based around licence-produced US rockets; ¤ Never flew an orbital flight (only 1 suborbital flight performed)
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Reduce both development period and costs by utilizing developed technologies as much as possible.
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The H-II was developed under the following policies, according to a NASDA press release:
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after F8 due to changes in schedule), and terminated the H-II series.
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The first and second stages of the canceled Flight 7, at a hangar in
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COMETS (Communications and
Broadcasting Engineering Test Satellites)
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ADEOS I (Advanced Earth
Observing Satellite) / Fuji OSCAR 29, JAS-2
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581:/LOX tanks, and a new upper stage, consisting of a cylindrical LH
715:(Orbital Re-entry Experiment), VEP (Vehicle Evaluation Payload)
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Develop a vehicle which can be launched from the existing
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Develop the launch vehicle with
Japanese space technology.
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H-II rocket at
Tsukuba science museum & planetarium
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in order to give Japan a capability to launch larger
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634:rockets started in order to minimize launch costs.
1007:The Ground Test Vehicle of H-II, now installed at
4051:Mitsubishi Heavy Industries space launch vehicles
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1129:Launch Vehicles and Space Transportation Systems
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606:(RSC), a consortium of 74 companies including
502:rocket following reliability and cost issues.
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964:MTSAT (Multi-functional Transport Satellite)
1721:Products currently in development shown in
585:tank with a capsule-shaped LOX tank. The LH
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880:TRMM (Tropical Rainfall Measuring Mission)
25:
577:The H-II was new, incorporating larger LH
494:in the 1990s. It was the first two-stage
4002:
1379:Nihon Aircraft Manufacturing Corporation
1068:Comparison of orbital launchers families
637:In 1996, RSC signed a contract with the
518:(the manufacturer of the Delta rockets,
757:ETS-VI (Engineering Test Satellite-VI)
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1098:(Press release). NASDA. Archived from
797:Geostationary Meteorological Satellite
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639:Hughes Space and Communications Group
1795:Comparison of orbital launch systems
1174:
1073:Comparison of orbital launch systems
1113:
652:List of H-II series and H3 launches
514:and its predecessors were from the
13:
1201:"Hughes cancels NASDA rocket deal"
1168:
14:
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1222:
903:Kiku 7 (Orihime & Hikoboshi)
886:(Engineering Test Satellite-VII)
645:
107:260,000 kg (570,000 lb)
1730:
1729:
1358:Mitsubishi Caterpillar Forklifts
1348:Japanese Aero Engine Corporation
1324:
1122:
1016:
1000:
4061:Expendable space launch systems
3623:Super heavy-lift launch vehicle
1709:Mitsubishi Sagamihara DynaBoars
1316:Mitsubishi Power Systems Europe
1298:Mitsubishi Aircraft Corporation
538:engine on the second stage and
136:10,060 kg (22,180 lb)
1790:List of orbital launch systems
1146:
1131:. JAXA Website. Archived from
626:. (This is in part due to the
351:1,078 kN (242,000 lb
305:1,540 kN (350,000 lb
1:
1078:
799:-5) / SFU (Space Flyer Unit)
505:
414:121.5 kN (27,300 lb
152:3,930 kg (8,660 lb)
7:
4056:Vehicles introduced in 1994
1651:Crystal Mover and Urbanismo
1273:Mitsubishi Heavy Industries
1175:Helm, Leslie (1992-07-13).
1154:"About H-II Launch Vehicle"
1032:
608:Mitsubishi Heavy Industries
428:452 s (4.43 km/s)
365:446 s (4.37 km/s)
319:273 s (2.68 km/s)
54:Mitsubishi Heavy Industries
10:
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3613:Medium-lift launch vehicle
1096:"H-II Launch Vehicle No.4"
993:
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604:Rocket Systems Corporation
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41:Medium-lift launch vehicle
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875:Yoshinobu Launch Complex
837:Yoshinobu Launch Complex
791:Yoshinobu Launch Complex
753:Yoshinobu Launch Complex
708:Yoshinobu Launch Complex
568:Tanegashima Space Center
540:inertial guidance system
482:) rocket was a Japanese
484:satellite launch system
91:49 m (161 ft)
1779:Orbital launch systems
1311:Mitsubishi FBR Systems
528:United Launch Alliance
3764:(Three stage variant)
1125:"H-II Launch Vehicle"
1045:H-II Transfer Vehicle
551:solid booster rockets
496:liquid-fuelled rocket
99:4 m (13 ft)
1306:Mitsubishi Logisnext
1051:H-II (rocket family)
1009:Tsukuba Space Center
1435:Mitsubishi SpaceJet
1229:H-II Launch Vehicle
1102:on 11 December 2003
1039:H-II Orbiting Plane
67:(sub, for the SRBs)
65:Alliant Techsystems
21:
2785:v1.2 "Full Thrust"
1234:2013-10-30 at the
696:TF1 (Test Flight)
261:Partial failure(s)
161:Associated rockets
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950:November 15, 1999
911:February 21, 1998
866:November 27, 1997
520:McDonnell Douglas
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75:Country of origin
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1468:Type 74 Nana-yon
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465:edit on Wikidata
424:Specific impulse
361:Specific impulse
315:Specific impulse
280:15 November 1999
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186:Derivative work
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16:Japanese rocket
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2296:
2286:
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2284:
2279:
2269:
2264:
2259:
2254:
2249:
2244:
2239:
2234:
2229:
2223:
2221:
2220:In development
2217:
2216:
2214:
2213:
2212:
2211:
2201:
2199:Vulcan Centaur
2196:
2195:
2194:
2184:
2179:
2174:
2169:
2164:
2163:
2162:
2157:
2152:
2142:
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2140:
2130:
2125:
2120:
2115:
2110:
2105:
2100:
2095:
2090:
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2078:
2073:
2068:
2063:
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2048:
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2016:
2011:
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2001:
1996:
1991:
1986:
1981:
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1971:
1966:
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1929:
1924:
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1872:
1867:
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1658:
1653:
1647:
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1640:
1638:
1637:
1632:
1627:
1622:
1620:Harushio class
1616:
1614:
1608:
1607:
1605:
1604:
1602:Takanami class
1599:
1594:
1592:Hatakaze class
1589:
1584:
1578:
1576:
1570:
1569:
1567:
1566:
1561:
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1376:
1370:
1368:
1364:
1363:
1361:
1360:
1355:
1350:
1344:
1342:
1335:
1334:Joint ventures
1331:
1330:
1323:
1321:
1319:
1318:
1313:
1308:
1303:
1294:
1292:
1286:
1285:
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1224:
1223:External links
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828:17 August 1996
826:
822:
821:
817:
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813:
811:
802:
800:
793:
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785:
780:
776:
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765:
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747:
744:28 August 1994
742:
738:
737:
736:Ryūsei, Myōjō
733:
732:
729:
727:
718:
716:
710:
705:
702:
697:
693:
692:
687:
684:
681:
678:
675:
672:
671:Configuration
667:
660:
650:Main article:
647:
646:Launch history
644:
598:
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582:
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458:
455:
454:
446:
442:
438:
437:
434:
430:
429:
426:
420:
419:
415:
412:
411:Maximum thrust
408:
407:
401:
397:
396:
392:
391:
383:
379:
375:
374:
371:
367:
366:
363:
357:
356:
352:
349:
348:Maximum thrust
345:
344:
338:
334:
333:
329:
328:
325:
321:
320:
317:
311:
310:
306:
303:
302:Maximum thrust
299:
298:
295:
291:
290:
286:
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281:
278:
274:
273:
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266:
265:
262:
258:
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250:
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246:
242:
241:
238:
237:Total launches
234:
233:
224:
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210:Launch history
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187:
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3527:
3524:
3522:
3519:
3515:
3512:
3510:
3507:
3505:
3502:
3500:
3499:UR-500 Proton
3497:
3496:
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3492:
3488:
3485:
3483:
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3478:
3475:
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3408:
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3321:
3318:
3317:
3316:
3313:
3311:
3308:
3306:
3303:
3301:
3298:
3296:
3293:
3291:
3288:
3286:
3285:Space Shuttle
3283:
3281:
3278:
3274:
3271:
3269:
3266:
3265:
3264:
3261:
3257:
3254:
3252:
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3214:
3212:
3209:
3207:
3204:
3202:
3199:
3197:
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3187:
3186:Blue Scout II
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3027:
3025:
3022:
3018:
3015:
3013:
3010:
3009:
3008:
3005:
3003:
3000:
2999:
2998:
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2990:
2988:
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2222:
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2197:
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2178:
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2119:
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2020:
2017:
2015:
2012:
2010:
2007:
2005:
2002:
2000:
1997:
1995:
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1911:
1908:
1907:
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1903:
1901:
1898:
1896:
1893:
1891:
1888:
1886:
1883:
1881:
1878:
1876:
1875:Firefly Alpha
1873:
1871:
1868:
1866:
1863:
1861:
1858:
1856:
1853:
1849:
1846:
1844:
1841:
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1834:
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1826:
1822:
1819:
1817:
1814:
1813:
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1809:
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1738:
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1728:
1727:
1724:
1720:
1719:
1716:
1710:
1707:
1706:
1704:
1700:
1694:
1693:Kazuo Tsukuda
1691:
1690:
1688:
1686:
1682:
1672:
1669:
1667:
1664:
1662:
1659:
1657:
1654:
1652:
1649:
1648:
1646:
1642:
1636:
1633:
1631:
1628:
1626:
1625:Oyashio class
1623:
1621:
1618:
1617:
1615:
1613:
1609:
1603:
1600:
1598:
1595:
1593:
1590:
1588:
1585:
1583:
1582:Akizuki class
1580:
1579:
1577:
1575:
1571:
1565:
1562:
1560:
1557:
1555:
1552:
1550:
1547:
1546:
1544:
1542:
1538:
1532:
1529:
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942:experiments.
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782:18 March 1995
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719:
717:
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709:
706:
703:
698:
694:
680:Payload mass
665:
662:Date / time (
657:
653:
643:
640:
635:
633:
629:
625:
619:
617:
613:
612:Nissan Motors
609:
605:
594:
592:
572:
569:
565:
562:
559:
558:
557:
554:
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548:
545:
541:
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521:
517:
516:Delta rockets
513:
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497:
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477:
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59:Nissan Motors
57:
55:
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51:
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28:
23:
3878:
3393:Thorad-Agena
3066:Soyuz/Vostok
2813:
1870:Falcon Heavy
1734:
1722:
1635:Taigei class
1515:
1290:Subsidiaries
1209:. Retrieved
1207:. 2000-05-26
1204:
1195:
1184:. Retrieved
1180:
1170:
1158:. Retrieved
1148:
1137:. Retrieved
1133:the original
1128:
1104:. Retrieved
1100:the original
674:Launch site
636:
628:Plaza Accord
620:
600:
576:
555:
509:
479:
475:
473:
395:Second stage
294:No. boosters
269:First flight
223:Launch sites
47:Manufacturer
2883:LauncherOne
2834:Kaituozhe-1
2611:Black Arrow
2363:Orbex Prime
2262:Hyperbola-2
2227:Antares 330
1927:Kaituozhe 2
1900:Hyperbola-1
1630:Sōryū class
1597:Kongō class
1587:Atago class
1473:Type 89 IFV
1160:12 December
820:Himawari 5
659:Flight No.
547:liquid-fuel
436:600 seconds
373:346 seconds
332:First stage
277:Last flight
245:Success(es)
227:Tanegashima
170:H-II family
141:Payload to
125:Payload to
4045:Categories
3892:NASDA/ISAS
2888:Long March
2792:Feng Bao 1
2405:Tianlong-3
2331:New Line 1
2289:Long March
2237:Cyclone-4M
2177:Tianlong-2
2155:2.1b / STB
2150:2.1a / STA
2093:Pegasus XL
1959:Long March
1932:Kinetica 1
1855:Chollima-1
1612:Submarines
1282:Mitsubishi
1211:2021-05-14
1186:2021-05-19
1139:2007-06-25
1106:2007-06-25
1079:References
985:Chichijima
506:Background
492:satellites
441:Propellant
400:Powered by
378:Propellant
337:Powered by
327:94 seconds
253:Failure(s)
200:Comparable
4003:Abandoned
3966:Space One
3736:Epsilon S
2987:Paektusan
2616:Conestoga
2373:Red Dwarf
2326:New Glenn
2257:Gravity-2
2247:Epsilon S
1880:Gravity-1
686:Customer
532:Delta III
433:Burn time
370:Burn time
324:Burn time
120:Capacity
3679:Japanese
3531:original
3521:Vanguard
3504:Proton-K
3477:original
3325:Ablestar
3310:Terran 1
3268:original
3127:Rocket 3
3034:original
2844:original
2770:Falcon 9
2765:Falcon 1
2721:IV Heavy
2437:Zuljanah
2400:Terran R
2383:Block 1B
2368:Pallas-1
2272:Kuaizhou
2232:Bloostar
2172:Starship
2123:Shavit 2
2108:Qaem 100
2098:Proton-M
2056:Minotaur
1937:Kuaizhou
1860:Electron
1828:Ariane 6
1736:Category
1671:Wakamaru
1541:Missiles
1402:Aircraft
1393:Products
1232:Archived
1033:See also
977:Failure
898:Success
853:Success
815:Success
769:Success
731:Success
691:outcome
677:Payload
669:Rocket,
593:engine.
526:and the
522:, later
289:Boosters
204:Ariane 4
176:Based on
96:Diameter
37:Function
3940:Planned
3899:Retired
3854:Retired
3785:Retired
3752:Epsilon
3745:Retired
3729:Planned
3682:orbital
3596:Classes
3467:Tsyklon
3305:Start-1
3076:Voskhod
3071:Sputnik
3007:Molniya
2992:Pilot-2
2829:Juno II
2743:Epsilon
2738:Energia
2728:Diamant
2604:Centaur
2453:Antares
2446:Retired
2395:Soyuz-7
2388:Block 2
2321:Neutron
2311:Miura 5
2145:Soyuz-2
2138:Block 1
2128:Simorgh
1905:Jielong
1833:Atlas V
1804:Current
1723:italics
1661:MEISTeR
1564:Type 91
1559:Type 90
1554:Type 89
1549:Type 88
1483:Type 10
1463:Type 61
1367:Defunct
1341:Current
1238:, JAXA.
994:Gallery
884:ETS-VII
795:GMS-5 (
774:Kiku 6
689:Launch
597:History
218:Retired
3981:KAIROS
3974:Active
3792:Lambda
3762:SS-520
3708:Active
3580:Zhuque
3514:Strela
3472:R-36-O
3415:II GLV
3403:SLV-2H
3398:SLV-2G
3386:DSV-2U
3364:Burner
3300:SS-520
3295:Sparta
3263:Shavit
3154:Saturn
3115:Shtil'
3081:Vostok
3024:Polyot
2982:Naro-1
2871:Lambda
2839:Kosmos
2824:Juno I
2748:Europa
2522:Athena
2485:Ariane
2425:Zhuque
2415:Vega E
2267:Irtysh
2204:Zhuque
1922:KAIROS
1811:Angara
1685:People
1430:MH2000
1156:. JAXA
1123:JAXA.
1041:(HOPE)
952:07:29
913:07:55
868:21:27
830:01:53
784:08:01
746:07:50
701:22:20
683:Orbit
624:Ariane
614:, and
524:Boeing
215:Status
166:Family
112:Stages
88:Height
3846:NASDA
3757:H-IIB
3715:H-IIA
3543:Zenit
3538:VLS-1
3509:Rokot
3410:Titan
3381:Delta
3342:Agena
3290:SPARK
3176:Scout
3132:Safir
3120:Volna
3029:Soyuz
2819:H-IIB
2733:Dnepr
2621:Delta
2599:Agena
2589:SLV-3
2584:LV-3B
2539:Atlas
2113:Qased
2088:OS-M1
1890:H-IIA
1838:Ceres
1702:Other
1644:Other
1574:Ships
1526:H-IIB
1521:H-IIA
1420:F-15J
1374:Atmea
1301:(90%)
1061:H-IIB
1056:H-IIA
1047:(HTV)
955:H-II
916:H-II
871:H-II
833:H-II
787:H-II
749:H-II
704:H-II
632:H-IIA
591:LE-5A
500:H-IIA
488:NASDA
463:[
405:LE-5A
231:LA-Y1
194:H-IIB
190:H-IIA
78:Japan
61:(sub)
3952:DECA
3947:ZERO
3879:H-II
3867:N-II
3826:3SII
3777:ISAS
3700:JAXA
3568:3SLB
3526:Vega
3455:CT-3
3440:IIIE
3435:IIID
3430:IIIC
3425:IIIB
3420:IIIA
3320:Able
3315:Thor
3216:X-2B
3206:X-3M
3196:X-2M
3110:R-29
3002:Luna
2977:N-II
2955:3SII
2854:2/2I
2814:H-II
2802:Mk I
2797:GSLV
2780:v1.1
2775:v1.0
2701:5000
2696:4000
2691:3000
2686:2000
2681:1000
2676:0100
2594:Able
2517:ASLV
2478:230+
2420:Zero
2346:OS-M
2341:Nova
2336:NGLV
2252:Eris
2242:Deca
2187:Vega
2182:Unha
2167:SSLV
2160:2-1v
2103:PSLV
2083:Nuri
2051:LVM3
1984:3B/E
1885:GSLV
1516:H-II
1506:N-II
1425:H-60
1162:2022
779:TF3
741:TF2
713:OREX
544:LE-7
536:LE-5
476:H-II
474:The
403:1 ×
342:LE-7
340:1 ×
149:Mass
133:Mass
104:Mass
83:Size
20:H-II
3932:IST
3906:J-I
3873:H-I
3861:N-I
3563:3SL
3558:2FG
3450:23G
3445:34D
3280:SLV
3256:G-1
3251:F-1
3246:E-1
3241:A-1
3236:D-1
3231:B-1
3211:X-4
3201:X-3
3191:X-2
3181:X-1
2997:R-7
2972:N-I
2809:H-I
2711:III
2579:III
2554:E/F
2473:230
2468:130
2463:120
2458:110
2410:VLM
2378:SLS
2316:MLV
2133:SLS
2118:RS1
2044:11H
1816:1.2
1511:H-I
1501:N-I
1445:X-2
1440:T-2
1415:F-2
1410:F-1
971:GEO
947:F8
930:GEO
908:F5
892:LEO
863:F6
847:LEO
825:F4
809:LEO
805:GEO
763:GEO
725:GTO
721:LEO
664:UTC
616:NEC
512:H-I
452:LOX
389:LOX
180:H-I
143:GTO
127:LEO
4047::
4010:GX
3821:3S
3816:3H
3811:3C
3806:4S
3802:Mu
3796:4S
3720:H3
3573:3F
3553:2M
3460:IV
3164:IB
3147:1B
3142:1A
3101:2M
3059:U2
3039:FG
2967:N1
2950:3S
2945:3H
2940:3C
2935:4S
2930:Mu
2923:4A
2918:3B
2908:2E
2903:2A
2898:1D
2876:4S
2864:3M
2758:II
2716:IV
2706:II
2574:II
2532:II
2304:12
2299:10
2282:31
2277:21
2066:IV
2039:11
2029:7A
2019:6A
2009:5B
1999:4C
1994:4B
1989:3C
1979:3A
1974:2F
1969:2D
1964:2C
1952:11
1947:1A
1895:H3
1848:1S
1821:A5
1531:H3
1203:.
1179:.
1127:.
1115:^
1087:^
987:.
882:/
807:/
723:/
666:)
610:,
480:H2
450:/
445:LH
387:/
382:LH
229:,
192:,
4012:‡
3908:¤
3875:‡
3869:‡
3863:‡
3833:)
3831:V
3804:(
3798:)
3794:(
3671:e
3664:t
3657:v
3585:1
3548:2
3487:3
3482:2
3374:2
3369:1
3357:D
3352:B
3347:A
3335:2
3330:1
3273:1
3226:A
3221:B
3169:V
3159:I
3137:1
3096:2
3091:K
3086:L
3054:U
3049:M
3044:L
3017:L
3012:M
2960:V
2913:3
2893:1
2859:3
2849:1
2753:I
2671:N
2666:M
2661:L
2656:J
2651:G
2646:E
2641:D
2636:C
2631:B
2626:A
2569:I
2564:H
2559:G
2549:D
2544:B
2527:I
2510:5
2505:4
2500:3
2495:2
2490:1
2430:3
2356:4
2351:2
2294:9
2209:2
2192:C
2076:C
2071:V
2061:I
2034:8
2024:7
2014:6
2004:5
1942:1
1915:3
1910:1
1843:1
1771:e
1764:t
1757:v
1265:e
1258:t
1251:v
1214:.
1189:.
1164:.
1142:.
1109:.
1027:.
1011:.
587:2
583:2
579:2
570:.
478:(
467:]
447:2
418:)
416:f
384:2
355:)
353:f
309:)
307:f
297:2
264:1
256:1
248:5
240:7
115:2
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