Top Qs
Timeline
Chat
Perspective

H-II Transfer Vehicle

Uncrewed cargo spacecraft developed by JAXA From Wikipedia, the free encyclopedia

H-II Transfer Vehicle
Remove ads


The H-II Transfer Vehicle (HTV), also called Kounotori (こうのとり, Kōnotori; "oriental stork" or "white stork"), was an expendable Japanese automated cargo spacecraft designed for International Space Station (ISS) resupply missions, particularly the Kibō Japanese Experiment Module (JEM).

Quick Facts Country of origin, Operator ...

Development of the spacecraft began in the early 1990s and the HTV's first mission, HTV-1, was launched on 10 September 2009 on an H-IIB launch vehicle.[4] The name Kounotori was chosen because "a white stork carries an image of conveying an important thing (a baby, happiness, and other joyful things), therefore, it precisely expresses the HTV's mission to transport essential materials to the ISS".[5]

The HTV was crucial for ISS resupply, especially after the retirement of the Space Shuttle, as it was the only vehicle capable of transporting large International Standard Payload Racks (ISPR) and disposing of old ones within the ISS's US Orbital Segment.

The final HTV mission, Kounotori 9, was launched on 20 May 2020. JAXA is developing its successor, the HTV-X, which is expected to make its maiden flight in 2025.

Remove ads

Design

Summarize
Perspective
Thumb
Structure
Thumb
The inside view of the Pressurised Logistics Carrier section of HTV-1.
Thumb
The Canadarm2 removing unpressurised payload from HTV-2.
Thumb
The four main thrusters. Smaller attitude control thrusters can be seen at the right side of this view of HTV-1.

The HTV was about 9.8 metres (32 ft) long (including maneuvering thrusters at one end) and 4.4 metres (14 ft) in diameter. Total mass when empty was 10,500 kilograms (23,100 lb), with a maximum total payload of 6,000 kilograms (13,000 lb), for a maximum launch weight of 16,500 kilograms (36,400 lb).[2]

The HTV was comparable in function to the Russian Progress, the ESA ATV, the SpaceX Cargo Dragons, and the Cygnus spacecraft, all of which brought supplies to the ISS. Like the ATV, the HTV carried more than twice the payload of the Progress, but was launched less than half as often. Unlike Progress spacecraft, Cargo Dragon 2's and ATV's which used the docking ports automatically, HTVs and American Dragon 1 approached the ISS in stages, and once they reached their closest parking orbit to the ISS, crew grappled them using the robotic arm Canadarm2 and berthed them to an open berthing port on the Harmony module.[6]

The HTV had an external payload bay which was accessed by the robotic arm after it had been berthed to the ISS. New payloads could be moved directly from the HTV to Kibō's exposed facility. Internally, it had eight International Standard Payload Racks (ISPRs) in total which could be unloaded by the crew in a shirt-sleeve environment. After the retirement of NASA's Space Shuttle in 2011, HTVs became the only spacecraft capable of transporting ISPRs to the ISS. The SpaceX Dragon and Northrop Grumman Cygnus could carry resupply cargo bags but not ISPRs.[citation needed]

The intent behind the HTV's modularized design was to use different module configurations to match different mission requirements.[7] However, to reduce the development cost it was decided to fly the mixed PLC/ULC configuration only.[7]

To control the HTV's attitude and perform the orbital maneuvers such as rendezvous and reentry, the craft had four 500-N-class main thrusters and twenty-eight 110-N-class attitude control thrusters. Both used bipropellant, namely monomethylhydrazine (MMH) as fuel and mixed oxides of nitrogen (MON3) as oxidizer.[8] HTV-1, HTV-2, and HTV-4 used Aerojet's 110 N R-1E, Space Shuttle's vernier engine, and the 500 N based on the Apollo spacecraft's R-4D.[8] Later HTVs used 500 N class HBT-5 thrusters and 120 N class HBT-1 thrusters made by Japanese manufacturer IHI Aerospace Co., Ltd.[9] The HTV's four spherical propellant tanks usually carried about 2 tonnes of propellant (the maximum capacity was 2432 kg[8]).

After the unloading process was completed, the HTV was loaded with waste and unberthed. The vehicle then deorbited and was destroyed during reentry, the debris felling into the Pacific Ocean.[10]

Remove ads

Flights

Summarize
Perspective
Thumb
The HTV-2 departing Tanegashima spaceport bound for the International Space Station.

Initially seven missions were planned between 2008–2015. With the extension of the ISS project through 2028, three more missions were added, with the tenth flight planned to debut an improved, cost-reduced version called the HTV-X.[11]

The first vehicle was launched on an H-IIB rocket, a more powerful version of the earlier H-IIA, at 17:01 UTC on 10 September 2009, from Launch Pad 2 of the Yoshinobu Launch Complex at the Tanegashima Space Center.[12]

By May 2020, all nine missions planned for HTV had been successfully launched, and the spacecraft was retired.

The improved HTV-X is planned to be first used for the tenth flight and will perform scheduled ISS resupply duties starting in 2025.[13]

More information HTV, Launch date/time (UTC) ...
Remove ads

Successor

Summarize
Perspective

HTV-X

In May 2015, Japan's Ministry of Education, Culture, Sports, Science and Technology announced a proposal to replace the HTV with an improved, cost-reduced version preliminary called HTV-X.[11][23]

In December 2015, the plan to develop HTV-X was approved by the Strategic Headquarters for Space Policy of the Cabinet Office, targeting launch in fiscal year 2021 for the flight of HTV-X1 (Technical Demonstration Vehicle) by the H3 rocket.[24][25] As of June 2019, new ISS plans from NASA's Flight Planning Integration Panel set the launch of HTV-X1 for February 2022.[26] In 2022 the debut of the HTV-X spacecraft was delayed to January 2024.[27]

The HTV-X has a length of 6.2 m, or 10 m with the unpressurised cargo module fitted. The payload fairing adaptor and payload dispenser have been widened from 1.7 m to 4.4 m to allow the pressurized cargo module to be swapped out for alternate modules, to add increased structural strength, and to accommodate the side hatch.[25]

As of 2021, an evolutionary version of HTV-X called HTV-XG was being considered for transferring cargo to the Lunar Gateway as part of the Artemis program.[28]

Former evolutionary proposals

Summarize
Perspective

HTV-R

As of 2010, JAXA was planning to add a return capsule option. In this concept, HTV's pressurized cargo would be replaced by a reentry module capable of returning 1,600 kilograms (3,500 lb) cargo from ISS to Earth.[29][30]

Further, conceptual plans in 2012 included a follow-on spacecraft design by 2022 which would accommodate a crew of three and carry up to 400 kilograms (880 lb) of cargo.[31]

Lagrange outpost resupply

As of 2014, both JAXA and Mitsubishi conducted studies of a next generation HTV as a possible Japanese contribution to the proposed international crewed outpost at Earth-Moon L2.[32][33] This variant of HTV was to be launched by H-X Heavy and can carry 1800 kg of supplies to EML2.[32] Modifications from the current HTV included the addition of solar electric paddles and extension of the propellant tank.[32]

Human-rated variant

A proposal announced in June 2008, "Preliminary Study for Manned Spacecraft with Escape System and H-IIB Rocket" suggested combining HTV's propulsion module with a human-rated capsule for four people.[34]

Japanese space station

A Japanese space station was proposed to be built up from HTV modules.[35] This method was similar to how the modules in Mir, as well as many modules of the Russian Orbital Segment of the ISS were based on the TKS cargo vehicle design.[citation needed]

Remove ads

See also

References

Loading related searches...

Wikiwand - on

Seamless Wikipedia browsing. On steroids.

Remove ads