Yoshinobu Launch Complex
Full view of the Yoshinobu Launch Complex during roll out of the H-IIA rocket in February 2014 | |||||||||||||||||||||||||
![]() Interactive map of Yoshinobu Launch Complex | |||||||||||||||||||||||||
| Launch site | Tanegashima | ||||||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Coordinates | 30°24′08″N 130°58′30″E / 30.40222°N 130.97500°E | ||||||||||||||||||||||||
| Short name | LA-Y | ||||||||||||||||||||||||
| Operator | JAXA, NASDA (former) | ||||||||||||||||||||||||
| Total launches | 75 | ||||||||||||||||||||||||
| Launch pad | 2 | ||||||||||||||||||||||||
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Yoshinobu Launch Complex (abbreviated LA-Y) is a rocket launch site at the Tanegashima Space Center on Tanegashima island in Japan.[1][2]
History
[edit]The Yoshinobu Launch Complex was built in the early 1990s to support launches of larger medium-lift launch vehicles, as the existing Osaki Launch Complex had been designed for small-lift launch vehicles. The Yoshinobu complex was initially developed for the H-II launch vehicle and has since supported launches of the H-IIA, H-IIB, and H3 rockets.[3]
Facilities
[edit]The complex consists of two launch pads:
- LA-Y1: previously used for H-II and H-IIA launches, planned to support H3 in the future
- LA-Y2: used for H3 launches, previously used for H-IIB launches
The site includes a vehicle assembly building (VAB), where launch vehicles delivered from manufacturing facilities are assembled, inspected, and prepared for launch. The building can accommodate the simultaneous assembly of two launch vehicles. Rockets are assembled atop a mobile launcher platform (ML), after which the payload and payload fairing are installed before rollout to the launch pad. The VAB is 81 metres (266 ft) tall, 64 metres (210 ft) wide, and 34.5 metres (113 ft) meters deep.[3][4] The rocket is transported to the launch pad about twelve hours before launch. Transport from the assembly building to pad takes approximately thirty minutes.[5]
The complex also contains the Yoshinobu Block House, located approximately 500 metres (1,600 ft) from the launch pads, next to the VAB. The launch control room is located 12 metres (39 ft) underground, where launch operations and countdown procedures are remotely monitored and controlled.[3]
The Yoshinobu Firing Test Stand is used for ground testing of first-stage rocket engines. It is currently used to test the LE-9 engine developed for the H3 launch vehicle.[3]
Launch statistics
[edit]LA-Y1
[edit]All launches until March 2003 operated by NASDA and Mitsubishi Heavy Industries. All launches afterwards operated by JAXA and Mitsubishi Heavy Industries.
| No. | Date | Time (UTC) | Launch vehicle | Configuration | Payload | Result | Remarks |
|---|---|---|---|---|---|---|---|
| 1 | 3 February 1994 | 22:20 | H-II | H-II | VEP-1 and OREX | Success | Maiden flight of the H-II family and from the Yoshinobu complex. Reentry demonstrator for OREX, testing various components to be used for the HOPE-X program.. |
| 2 | 28 August 1994 | 07:50 | H-II | H-II | ETS-VI | Success | |
| 3 | 18 March 1995 | 08:01 | H-II | H-II | GMS-5 and Space Flyer Unit | Success | Space Flyer Unit was retrieved and returned to Earth by Space Shuttle Endeavour in 1996, as part of STS-72. |
| 4 | 17 August 1996 | 01:53 | H-II | H-II | ADEOS I, Fuji-OSCAR 29, and JAS-2 | Success | |
| 5 | 27 November 1997 | 21:27 | H-II | H-II | Tropical Rainfall Measuring Mission and ETS-VII | Success | Part of Mission to Planet Earth for TRMM, designed to study precipitation in the tropics. Collaboration between JAXA and NASA. |
| 6 | 21 February 1998 | 07:55 | H-II | H-II | COMETS | Partial failure | Cooling system issues led to premature second stage engine shutdown during geostationary transfer burn, leaving payload stranded in low Earth orbit. Onboard thrusters compensated and allowed for some operations to proceed. |
| 7 | 15 November 1999 | 07:29 | H-II | H-II | MTSAT-1 | Failure | Part of the Himawari series of geostationary weather satellites. Impeller failure led to premature engine shutdown 239 seconds after launch, leading to failure to achieve orbit. Final launch of the baseline H-II. |
| 8 | 29 August 2001 | 07:00 | H-IIA | H-IIA 202 | VEP-2 | Success | Maiden flight of the H-IIA. Carried boilerplate payload. |
| 9 | 4 February 2002 | 02:45 | H-IIA | H-IIA 2024 | VEP-3 and MDS-1 | Success | |
| 10 | 10 September 2002 | 08:20 | H-IIA | H-IIA 2024 | USERS and DRTS | Success | |
| 11 | 14 December 2002 | 01:31 | H-IIA | H-IIA 202 | ADEOS II, WEOS, FedSat 1, and Micro LabSat 1 | Success | |
| 12 | 28 March 2003 | 01:27 | H-IIA | H-IIA 2024 | IGS-Optical 1 and IGS-Radar 1 | Success | |
| 13 | 29 November 2003 | 04:33 | H-IIA | H-IIA 2024 | IGS-Optical 2 and IGS-Radar 2 | Failure | Gas leak led to failure of a solid rocket booster jettison, with added weigh leading to failure to achieve orbit. |
| 14 | 26 February 2005 | 09:25 | H-IIA | H-IIA 2022 | MTSAT-1R | Success | Part of the Himawari series of geostationary weather satellites. |
| 15 | 24 January 2006 | 01:33 | H-IIA | H-IIA 2022 | ALOS | Success | |
| 16 | 18 February 2006 | 06:27 | H-IIA | H-IIA 2024 | MTSAT-2 | Success | Part of the Himawari series of geostationary weather satellites. |
| 17 | 11 September 2006 | 04:35 | H-IIA | H-IIA 202 | IGS-Optical 2 | Success | |
| 18 | 18 December 2006 | 06:32 | H-IIA | H-IIA 204 | ETS-VIII | Success | |
| 19 | 24 February 2007 | 04:41 | H-IIA | H-IIA 2024 | IGS-Radar 2 and IGS-Optical 3V | Success | |
| 20 | 14 September 2007 | 01:31 | H-IIA | H-IIA 2022 | SELENE | Success | Also known as Kaguya, designed to explore the Moon. Second spacecraft from Japan to enter lunar orbit, after Hiten. First launch from Tanegashima to another celestial body. |
| 21 | 23 February 2008 | 08:55 | H-IIA | H-IIA 2024 | WINDS | Success | |
| 22 | 23 January 2009 | 03:54 | H-IIA | H-IIA 202 | GOSAT and others | Success | First satellite dedicated to the observation of greenhouse gases. |
| 23 | 28 November 2009 | 01:21 | H-IIA | H-IIA 202 | IGS-Optical 3 | Success | |
| 24 | 20 May 2010 | 21:58 | H-IIA | H-IIA 202 | Akatsuki, IKAROS, and others | Success | Part of the PLANET series of spacecraft fort Akatsuki, designed to explore Venus and study its atmosphere. Failed to initially enter Venusian orbit in 2010, but managed to return and successfully entered orbit in 2015. First successful demonstration of solar sail technology beyond LEO for IKAROS. First launch from Tanegashima to enter heliocentric orbit. |
| 25 | 11 September 2010 | 11:17 | H-IIA | H-IIA 202 | QZS-1 | Success | |
| 26 | 23 September 2011 | 04:36 | H-IIA | H-IIA 202 | IGS-Optical 4 | Success | |
| 27 | 12 December 2011 | 01:21 | H-IIA | H-IIA 202 | IGS-Radar 3 | Success | |
| 28 | 17 May 2012 | 16:39 | H-IIA | H-IIA 202 | GCOM-W1, KOMPSAT-3, SDS-4, and HORYU-2 | Success | |
| 29 | 27 January 2013 | 04:40 | H-IIA | H-IIA 202 | IGS-Radar 4 and IGS-Optical 5V | Success | |
| 30 | 27 February 2014 | 18:37 | H-IIA | H-IIA 202 | Global Precipitation Measurement and others | Success | Collaboration between JAXA and NASA. Successor to TPMM, designed to make frequent observations of rainfall. |
| 31 | 24 May 2014 | 03:05 | H-IIA | H-IIA 202 | ALOS-2 and others | Success | |
| 32 | 7 October 2014 | 05:16 | H-IIA | H-IIA 202 | Himawari 8 | Success | Part of the Himawari series of geostationary weather satellites. |
| 33 | 3 December 2014 | 04:22 | H-IIA | H-IIA 202 | Hayabusa2 and others | Success | Sample-return mission, designed to collect asteroid sediment from 162173 Ryugu and return it to Earth. Successor to the previous Haybusa mission. |
| 34 | 1 February 2015 | 01:21 | H-IIA | H-IIA 202 | IGS-Radar Spare | Success | |
| 35 | 26 March 2015 | 01:21 | H-IIA | H-IIA 202 | IGS-Optical 5 | Success | |
| 36 | 24 November 2015 | 06:50 | H-IIA | H-IIA 204 | Telstar 12 Vantage | Success | |
| 37 | 17 February 2016 | 08:45 | H-IIA | H-IIA 202 | Hitomi and others | Success | Space telescope designed to conduct x-ray astronomy. Launch was a success, but attitude control problems led to spacecraft failure 37 days after launch. |
| 38 | 2 November 2016 | 06:20 | H-IIA | H-IIA 202 | Himawari 9 | Success | Part of the Himawari series of geostationary weather satellites. |
| 39 | 24 January 2017 | 07:44 | H-IIA | H-IIA 204 | DSN-2 | Success | |
| 40 | 17 March 2017 | 01:20 | H-IIA | H-IIA 202 | IGS-Radar 5 | Success | |
| 41 | 1 June 2017 | 00:17 | H-IIA | H-IIA 202 | QZS-2 | Success | |
| 42 | 19 August 2017 | 05:29 | H-IIA | H-IIA 204 | QZS-3 | Success | |
| 43 | 9 October 2017 | 22:01 | H-IIA | H-IIA 202 | QZS-4 | Success | |
| 44 | 23 December 2017 | 01:26 | H-IIA | H-IIA 202 | GCOM-C and SLATS | Success | |
| 45 | 27 February 2018 | 04:34 | H-IIA | H-IIA 202 | IGS-Optical 6 | Success | |
| 46 | 12 June 2018 | 04:20 | H-IIA | H-IIA 202 | IGS-Radar 6 | Success | |
| 47 | 29 October 2018 | 04:08 | H-IIA | H-IIA 202 | GOSAT-2 and others | Success | |
| 48 | 9 February 2020 | 01:34 | H-IIA | H-IIA 202 | IGS-Optical 7 | Success | |
| 49 | 19 July 2020 | 21:58 | H-IIA | H-IIA 202 | Emirates Mars Mission | Success | Also known as Hope, designed to explore Mars. Made the United Arab Emirates the fifth nation to enter areocentric orbit. Final H-II series launch into interplanetary space. |
| 50 | 29 November 2020 | 07:25 | H-IIA | H-IIA 202 | JDRS/LUCAS | Success | |
| 51 | 26 October 2021 | 02:19 | H-IIA | H-IIA 202 | QZS-1R | Success | |
| 52 | 22 December 2021 | 15:32 | H-IIA | H-IIA 204 | Inmarsat-6 F1 | Success | |
| 53 | 26 January 2023 | 01:50 | H-IIA | H-IIA 202 | IGS-Radar 7 | Success | |
| 54 | 6 September 2023 | 23:42 | H-IIA | H-IIA 202 | XRISM and SLIM | Success | Collaboration between NASA, ESA, and JAXA for XRISM, a space telescope designed to perform x-ray astronomy. Lunar lander for SLIM, making Japan the fifth nation to successfully land on the Moon. Also set non-RTG record for staying operational on the Lunar surface, at 3 months and 10 days. Final H-II series launch beyond LEO. |
| 55 | 12 January 2024 | 04:44 | H-IIA | H-IIA 202 | IGS-Optical 8 | Success | |
| 56 | 26 September 2024 | 05:24 | H-IIA | H-IIA 202 | IGS-Radar 8 | Success | |
| 57 | 28 June 2025 | 16:33 | H-IIA | H-IIA 202 | GOSAT-GW | Success | Final launch of the H-IIA, and last flight of an H-II series launch vehicle. |
LA-Y2
[edit]All flights operated by JAXA and Mitsubishi Heavy Industries.
| No. | Date | Time (UTC) | Launch vehicle | Configuration | Payload | Result | Remarks |
|---|---|---|---|---|---|---|---|
| 1 | 10 September 2009 | 17:01 | H-IIB | H-IIB | HTV Demonstration Flight | Success | Maiden flight of the H-IIB and from LA-Y2. First launch of the H-II Transfer Vehicle, going to the International Space Station. Made Tanegashima the fourth launch site (after Baikonur, Cape Canaveral/KSC, and Kourou) to send a payload to the ISS. |
| 2 | 22 January 2011 | 05:37 | H-IIB | H-IIB | Kounotori 2 | Success | ISS resupply flight. |
| 3 | 21 July 2012 | 02:06 | H-IIB | H-IIB | Kounotori 3 | Success | ISS resupply flight. |
| 4 | 3 August 2013 | 19:48 | H-IIB | H-IIB | Kounotori 4 | Success | ISS resupply flight. |
| 5 | 19 August 2015 | 11:50 | H-IIB | H-IIB | Kounotori 5 | Success | ISS resupply flight. |
| 6 | 9 December 2016 | 13:26 | H-IIB | H-IIB | Kounotori 6 | Success | ISS resupply flight. |
| 7 | 22 September 2018 | 17:52 | H-IIB | H-IIB | Kounotori 7 | Success | ISS resupply flight. |
| 8 | 24 September 2019 | 16:05 | H-IIB | H-IIB | Kounotori 8 | Success | ISS resupply flight. |
| 9 | 20 May 2020 | 17:31 | H-IIB | H-IIB | Kounotori 9 | Success | ISS resupply flight. Final H-IIB launch and last flight of the H-II Transfer Vehicle. |
| 10 | 7 March 2023 | 01:37 | H3 | H3‑22S | ALOS-3 | Failure | Maiden flight of the H3. Electrical circuit failure caused second stage engine to not ignite, leading to failure of placing payload into orbit. |
| 11 | 17 February 2024 | 00:22 | H3 | H3‑22S | VEP-4 | Success | First successful H3 launch. Boilerplate payload, plus carried two rideshares. |
| 12 | 1 July 2024 | 03:06 | H3 | H3‑22S | ALOS-4 | Success | |
| 13 | 4 November 2024 | 06:48 | H3 | H3‑22S | DSN-3 | Success | |
| 14 | 2 February 2025 | 08:30 | H3 | H3‑22S | QZS-6 | Success | |
| 15 | 26 October 2025 | 00:00 | H3 | H3-24W | HTV-X1 | Success | First launch of the HTV-X spacecraft, going to the International Space Station. |
| 16 | 22 December 2025 | 01:51 | H3 | H3‑22S | QZS-5 | Failure | Payload support structure failed during fairing separation, leading to loss of payload before vehicle made orbit. |
| 17 | 12 June 2026 | 00:53 | H3 | H3‑30S | VEP-5 | Success | Boilerplate payload, plus carried six rideshares. |
| 18 | 10 August 2026 | 19:23 | H3 | H3‑22S | QZS-7 | Success |
Upcoming launches
[edit]| Date | Launch vehicle | Payload |
|---|---|---|
| 19 October 2026 | H3 | Martian Moons eXploration |
See also
[edit]References
[edit]- ↑ "Tanegashima Y". astronautix.com. Archived from the original on 28 December 2016. Retrieved 30 May 2020.
- ↑ "Tanegashima Space Center (TNSC)". JAXA. Archived from the original on 8 December 2006. Retrieved 19 January 2009.
- 1 2 3 4 "Tanegashima Space Center brochure" (PDF). JAXA. June 2023. Retrieved 8 May 2026.
- ↑ "Launch Preparation Report". H-IIA Launch Services Flight 15. Mitsubishi Heavy Industries. 16 January 2009. Archived from the original on 30 January 2009. Retrieved 19 January 2009.
- ↑ "Countdown Report". H-IIA Launch Vehicle 14. Mitsubishi Heavy Industries. 23 February 2008. Archived from the original on 4 March 2016. Retrieved 19 January 2009.
