H-II Transfer Vehicle
Role: Uncrewed spacecraft intended to resupply the
on the Kibō Japanese Experiment Module International Space Station and, if necessary, the rest of the station.
Height: ~9.8 m (including thrusters)
Diameter: 4.4 m
Spacecraft Mass: 10,500 kg
Total Launch Payload: 6,000 kg
Pressurized Payload: 5,200 kg
Unpressurized Payload: 1,500 kg
Return Payload: None
Mass at launch: 16.5 ton
Pressurized Volume: 14 m
3 [4 ]
Endurance: Solo flight about 100 hours, stand-by more than a week, docked with the ISS about 30 days
Apogee: 460 km
Perigee: 350 km
Inclination: 51.6 degrees
H-II Transfer Vehicle ( HTV), also called Kounotori (, is an こうのとり Kōnotori, " Oriental Stork" or " White Stork") automated resupply spacecraft used to resupply the (JEM) and the Kibō Japanese Experiment Module International Space Station (ISS). The Japan Aerospace Exploration Agency (JAXA) has been working on the design since the early 1990s. The first mission, HTV-1, was originally intended to be launched in 2001. It launched at 17:01 UTC on 10 September 2009 on an H-IIB launch vehicle. The name [5 ] Kounotori was chosen for the HTV by JAXA 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". [6 ]
Inside view of the Pressurised Logistics Carrier section of HTV-1.
Canadarm2 removing unpressurised payload from HTV-2.
The HTV is about 9.8 m long (including maneuvering thrusters at one end) and 4.4 m in diameter. Total mass is 10.5 tonnes, with a 6,000 kilograms (13,000 lb) payload.
The HTV are comparable in function to the [1 ] Russian Progress, European ATV, commercial Dragon, and commercial Cygnus spacecraft, all of which bring or are planned to bring supplies to the ISS. Like the ATV, the HTV carries more than twice the payload of the Progress, but is launched less than half as often. Unlike Progress capsules and ATVs, which dock automatically, HTVs and American commercial crafts approach the ISS in stages, and are signaled by ISS crew or ground control to continue from one holding point to the next. Once they reach their closest parking orbit to the ISS, crew grip them using the robotic arm Canadarm2 and berth them to an open berthing port on the module. Harmony [7 ]
The HTV has an external payload bay which is accessed by robotic arm after it has been berthed to the ISS. New payloads can be moved directly from the HTV to
s exposed facility. Internally, it has eight Kibō' International Standard Payload Racks (ISPRs) in total which can 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 Orbital Sciences Cygnus can carry resupply cargo bags but not ISPRs.)
The four main thrusters. Smaller attitude control thrusters can be seen at the right side of this view of HTV-1.
The baseline configuration, known as the "Mixed Logistics Carrier", uses one pressurized and one unpressurized segment and can carry 7,600 kg of cargo in total and is 9.2 m long. When two pressurized units are used together the cargo decreases slightly to about 7,000 kg, and the overall length is reduced to 7.4 m.
To control the HTV's attitude and to perform the orbital maneuvers such as rendezvous and re-entry, the craft has four 500 N class main thrusters and twenty-eight 110 N class attitude control thrusters. Both use bipropellant, namely
monomethylhydrazine (MMH) as fuel and mixed oxides of nitrogen (MON3) as oxidizer. HTV-1, -2, and -4 use [9 ] Aerojet's 110 N R-1E, Space Shuttle's vernier engine, and the 500 N based on the Apollo spacecraft's R-4D. Later HTVs use 500 N class [9 ] HBT-5 thrusters and 120 N class HBT-1 thrusters made by Japanese manufacturer IHI Aerospace Co., Ltd. The HTV carries about 2400 kg of propellant in four tanks. [10 ] [9 ]
After the unloading process is completed, the HTV will be loaded with waste and undocked. The vehicle will then deorbit and be destroyed during reentry, the debris falling into the
Pacific Ocean. [3 ]
As of 2010
[11 ] It is expected to be launched by 2018. [12 ] [13 ]
, JAXA is planning to add a return capsule option. HTV's Pressurized Cargo is replaced by a reentry module capable of returning 1.6 tonne cargo from ISS to Earth.
Further, it is expected to be followed on by 2022 by capsules which accommodate a crew of three and carry up to 880 pounds (400 kilograms) of cargo.
Flights [ edit ]
HTV-2 departing Tanegashima spaceport bound for the International space station
The first vehicle was launched on an
H-IIB rocket, a more powerful version of the earlier H-IIA, at 17:01 GMT on 10 September 2009, from Launch Pad 2 of the Yoshinobu Launch Complex at the Tanegashima Space Center. Six subsequent missions are planned. [15 ] [16 ]
Launch date/time (
UTC) Berth date/time (UTC)
[17 ] Carrier rocket
HTV-1 10 September 2009, 17:01:56
17 September 2009, 22:12
H-IIB F1 1 November 2009, 21:26
HTV-2 22 January 2011, 05:37:57
27 January 2011, 14:51
H-IIB F2 30 March 2011, 03:09
HTV-3 21 July 2012, 02:06:18
27 July 2012, 14:34
H-IIB F3 14 September 2012, 05:27
HTV-4 3 August 2013, 19:48:46
9 August 2013, 15:38
H-IIB F4 [20 ] 7 September 2013, 06:37
HTV-5 February 2015
[16 ] [22 ]
HTV-6 February 2016
[16 ] [23 ]
See also [ edit ]
References [ edit ]
^ a b c d e f g h "H-II Transfer Vehicle "KOUNOTORI" (HTV)". Japan Aerospace Exploration Agency. 2007 . Retrieved 2010-11-11.
^ a b c d Overview of the "KOUNOTORI". Japan Aerospace Exploration Agency. Retrieved 2011-01-18.
^ a b JAXA (2007). "HTV Operations" . Retrieved 2011-01-02.
^ "JAXA H-II Transfer Vehicle (HTV)". NASA . Retrieved 8 December 2013.
^ "NASA Sets Briefing, TV Coverage of Japan's First Cargo Spacecraft". NASA . Retrieved 2009-09-03.
^ ". JAXA. 11 November 2010 "KOUNOTORI" Chosen as Nickname of the H-II Transfer Vehicle (HTV)" . Retrieved 11 November 2010.
^ http://www.abo.fi/~mlindroo/Station/Slides/sld098a.htm - NASDA H-II Transfer Vehicle
^ a b c IAC paper IAC-05-C4.1.03 - Shinobu Matsuo and al. "The design characteristics of the HTV propulsion module"
^ "宇宙ステーション補給機「こうのとり」3号機（HTV3）ミッションプレスキット" (in Japanese). June 20, 2012 . Retrieved June 24, 2012.
^ "回収機能付加型宇宙ステーション補給機（HTV-R）検討状況" (in Japanese). JAXA. August 11, 2011 . Retrieved September 7, 2011.
^ "回収機能付加型HTV(HTV-R)" (in Japanese). JAXA . Retrieved September 7, 2011.
^ "JAXAでは宇宙ステーション補給機「こうのとり」（HTV）への回収機能の付加について研究を行っています。" (in Japanese). JAXA. September 7, 2011 . Retrieved 9 August 2013.
^ Rob Coppinger. "Japan Wants Space Plane or Capsule by 2022". Space.com . Retrieved October 25, 2012.
^ Launch of the H-IIB Launch Vehicle Test Flight, JAXA Press release, 8 July 2009 (JST)
^ a b c d "International Space Station Flight Schedule". SEDS. 15 May 2013 . Retrieved 9 August 2013.
^ "H-II Transfer Vehicle "KOUNOTORI" (HTV) Topics". Japan Aerospace Exploration Agency.
^ Stephen Clark (1 November 2009). "History-making Japanese space mission ends in flames". Spaceflight Now . Retrieved 13 November 2010.
^ Stephen Clark (29 March 2011). "Japan's HTV cargo freighter proves useful to the end". Spaceflight Now . Retrieved 21 April 2011.
^ Stephen Clark (3 August 2013). "Japan launches resupply mission to space station". Spaceflight Now . Retrieved 3 August 2013.
^ Stephen Clark (9 August 2013). "JJapan's cargo craft makes in-orbit delivery to space station". Spaceflight Now . Retrieved 9 August 2013.
^ "JAXA Launch Schedule". JAXA . Retrieved 3 August 2013.
^ "Schedule of ISS flight events (part 1)". NASA Spaceflight.com . Retrieved 4 August 2013.
External links [ edit ]