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46 relations: Akita Prefecture, ArduSat, Ōdate, Battleship (rocketry), Comparison of orbital launch systems, Comparison of orbital launchers families, Coordinated Universal Time, CubeSat, Expendable launch system, F-1 (satellite), Falcon 9 Full Thrust, Geostationary transfer orbit, GTO, H-II Transfer Vehicle, H-IIA, HTV-1, Hydroxyl-terminated polybutadiene, International Space Station, JAXA, Kounotori 2, Kounotori 3, Kounotori 4, Kounotori 5, Kounotori 6, LE-5, LE-7, Leo, Liquid hydrogen, Liquid oxygen, List of H-I and H-II launches, Low Earth orbit, Medium-lift launch vehicle, Mitsubishi Heavy Industries, Modular rocket, Niwaka, PicoDragon Satellite, Polybutadiene, Proton-M, Raiko, Rocket, Solid-propellant rocket, SRB-A, Tanegashima Space Center, TechEdSat, We-Wish, Yoshinobu Launch Complex.
Akita Prefecture
is a prefecture located in the Tōhoku region of Japan.
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ArduSat
ArduSat is an Arduino based Nanosatellite, based on the CubeSat standard.
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Ōdate
is a city in Akita Prefecture, Japan.
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Battleship (rocketry)
In rocketry, a battleship was a term used during the design of the Saturn V to refer to a heavy duty rocket stage which was used to test configuration and integration of a launch vehicle.
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Comparison of orbital launch systems
This is a comparison of orbital launch systems.
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Comparison of orbital launchers families
This page contains a list of orbital launchers' families.
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Coordinated Universal Time
No description.
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CubeSat
A CubeSat (U-class spacecraft) is a type of miniaturized satellite for space research that is made up of multiples of 10×10×10 cm cubic units.
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Expendable launch system
An expendable launch vehicle (ELV) is a launch system or launch vehicle stage that is used only once to carry a payload into space.
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F-1 (satellite)
F-1 is a 1U CubeSat built by FSpace laboratory at FPT University in Vietnam, in partnership with, Uppsala University and NanoRacks LLC.
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Falcon 9 Full Thrust
Falcon 9 Full Thrust (also known as Falcon 9 v1.2, with Block 3, Block 4 and Block 5 variants) is a partially reusable medium-lift launch vehicle, designed and manufactured by SpaceX.
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Geostationary transfer orbit
A geosynchronous transfer orbit or geostationary transfer orbit (GTO) is a Hohmann transfer orbit—an elliptical orbit used to transfer between two circular orbits of different radii in the same plane—used to reach geosynchronous or geostationary orbit using high-thrust chemical engines.
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GTO
GTO may refer to.
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H-II Transfer Vehicle
The H-II Transfer Vehicle (HTV), also called, is an automated cargo spacecraft used to resupply the ''Kibō'' Japanese Experiment Module (JEM) and the International Space Station (ISS).
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H-IIA
H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency.
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HTV-1
HTV-1, also known as the HTV Demonstration Flight or HTV Technical Demonstration Vehicle, was the first Japanese Space Agency (JAXA) H-II Transfer Vehicle, launched in September 2009 to resupply the International Space Station and support the JAXA Kibo (きぼう, Kibō?, Hope) laboratory or JEM.
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Hydroxyl-terminated polybutadiene
Hydroxyl-terminated polybutadiene (HTPB) is an oligomer of butadiene terminated at each end with a hydroxyl functional group.
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International Space Station
The International Space Station (ISS) is a space station, or a habitable artificial satellite, in low Earth orbit.
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JAXA
The is the Japanese national aerospace and space agency.
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Kounotori 2
Kounotori 2 (こうのとり2号機, "white stork"), also known as HTV-2, was launched in January 2011 and was the second Japanese H-II Transfer Vehicle to resupply the International Space Station (ISS).
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Kounotori 3
Kounotori 3 (こうのとり3号機; English: "white stork"), also known as HTV-3, is the third Japanese H-II Transfer Vehicle.
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Kounotori 4
Kounotori 4, also known as HTV-4, was the fourth flight of the H-II Transfer Vehicle, an unmanned cargo spacecraft launched in August 2013 to resupply the International Space Station.
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Kounotori 5
Kounotori 5, also known as HTV-5, is the fifth flight of the H-II Transfer Vehicle, an uncrewed cargo spacecraft launched to resupply the International Space Station.
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Kounotori 6
, also known as HTV-6, is the sixth flight of the H-II Transfer Vehicle, an unmanned cargo spacecraft launched to resupply the International Space Station.
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LE-5
The LE-5 liquid rocket engine and its derivative models were developed in Japan to meet the need for an upper stage propulsion system for the H-I and H-II series of launch vehicles.
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LE-7
The LE-7 and its succeeding upgrade model the LE-7A are staged combustion cycle LH2/LOX liquid rocket engines produced in Japan for the H-II series of launch vehicles.
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Leo
Leo, the Latin word for "lion", or LEO may refer to.
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Liquid hydrogen
Liquid hydrogen (LH2 or LH2) is the liquid state of the element hydrogen.
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Liquid oxygen
Liquid oxygen—abbreviated LOx, LOX or Lox in the aerospace, submarine and gas industries—is one of the physical forms of elemental oxygen.
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List of H-I and H-II launches
This is a list of launches made by JAXA using H-I, H-II, H-IIA, and H-IIB rockets.
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Low Earth orbit
A low Earth orbit (LEO) is an orbit around Earth with an altitude of or less, and with an orbital period of between about 84 and 127 minutes.
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Medium-lift launch vehicle
A medium-lift launch vehicle - MLV a rocket orbital launch vehicle that is capable of lifting between of payload into Low Earth orbit - LEO.
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Mitsubishi Heavy Industries
is a Japanese multinational engineering, electrical equipment and electronics company headquartered in Tokyo, Japan.
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Modular rocket
A modular rocket is a type of multistage rocket which features components that can be interchanged for specific mission requirements.
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Niwaka
Niwaka or FITSAT-1 is a 1U CubeSat satellite deployed from the International Space Station on October 4, 2012.
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PicoDragon Satellite
PicoDragon is a small satellite that followed the 1U of CubeSat program built by Vietnam National Satellite Center belong to VAST and operated in space for 3 months.
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Polybutadiene
Polybutadiene is a synthetic rubber.
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Proton-M
The Proton-M, (Протон-М) GRAU index 8K82M or, is a Russian heavy-lift launch vehicle derived from the Soviet-developed Proton.
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Raiko
Raiko (雷鼓, literally thunder drum) is a Japanese satellite which was built and operated by Tohoku and Wakayama Universities.
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Rocket
A rocket (from Italian rocchetto "bobbin") is a missile, spacecraft, aircraft or other vehicle that obtains thrust from a rocket engine.
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Solid-propellant rocket
A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer).
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SRB-A
SRB-A is a series of Japanese solid-fueled rocket booster manufactured by IHI Corporation for use on the H-IIA, H-IIB, and Epsilon rockets.
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Tanegashima Space Center
The (TNSC) is a Japanese space development facility.
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TechEdSat
The Technological and Educational Nanosatellite, or TechEdSat, is a series of CubeSats built by San Jose State University and University of Idaho students in partnership with Ames Research Center and ÅAC Microtec.
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We-Wish
We-Wish was a small commercial CubeSat which was deployed from the International Space Station (ISS) in October 2012 and which deorbited in March 2013.
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Yoshinobu Launch Complex
The Yoshinobu Launch Complex, also known as Launch Area Y, Area Y or LA-Y, is a launch complex at the Tanegashima Space Centre, located on Tanegashima, the Japanese island located 115 km south of Kyūshū.
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Redirects here:
H-2B, H-IIB rocket, H2-B.
References
[1] https://en.wikipedia.org/wiki/H-IIB
