Rocket Systems and Space Exploration
IHI has participated in Japan’s space development effort from the outset. We have applied our cryogenic-pump and turbomachinery and other technologies to develop and manufacture the turbopumps and gas-jet systems crucial to successful rocket launches. Our involvement in Japan’s space program expanded significantly in 2000, when we acquired Nissan Motor’s Aerospace Division, a pioneer in solid-fuel rocket development in Japan. We play an important role in developing and constructing the Exposed Facilities of the KIBO Japanese Experiment Module, which is a part of the International Space Station program. We support experiments in space by supplying experimental systems needed for cooperative international projects.
H-IIA rocket／H-IIB rocket
H-IIA rocket／H-IIB rocket,IHI group is developing and producing the turbopumps, solid rocket boosters（SRB-A）, 2-stage gas-jet, and the pyrotechnic materials.
The M-V rocket is one of the world's largest 3-stage solid fuel rocket with a diameter of 2.51 m and it is capable of launching a satellite weighing approximately 1.8 tons into a low-altitude orbit. The M-V rocket has been used to launch satellites developed for space exploration (1997-2006).
Epsilon launch vehicle
The Epsilon launch vehicle is a new rocket, based on the M-V launch vehicle, being developed to provide a more reliable, and responsive space launch system with a lower life-cycle cost for various small satellites customers.
The first flight is scheduled in FY2013.
Development of LNG propulsion system
LNG propulsion system , which uses LNG (Liquefied Natural Gas) as a fuel, has advantages of better storability in space and higher density than Hydrogen. By taking these merits, LNG propulsion system can be applied for future project of orbit transfer vehicle and planetary probe mission.
Rocket Propulsion Systems
Liquid oxygen turbopump for the H-IIA rocket / LE-7A engine
This pump supplies the liquid oxygen needed to burn the hydrogen fuel in the rocket engines. Together with the liquid hydrogen turbopump, it forms the heart of the rocket.
Liquid hydrogen turbopump for the H-IIA rocket / LE-7A engine
This pump supplies the liquid hydrogen fueling the rocket engines. This forms the heart of the rocket. IHI provides the turbopumps for both the first-stage LE-7A engine and the second-stage LE-5B engine.
Satellite Propulsion Systems
Development of bipropellant liquid apogee engine, etc., used to obtain geostationary orbit
The apogee engine with 500 N class thrust developed by IHI group has the highest level of performance in the world, rated as top by the clients all over the world along with the 22N thruster.
Systems for Satellites
Monitor Camera for Spacecraft
The monitor camera is a unit consisting of a floodlight (left), a camera (right) and a camera controller to take pictures of deployments of satellite-mounted solar battery paddles and antennas.
Transceiver for Spacecraft
It will be installed on the small satellite and perform the command reception from the ground, and the telemetry transmission to the ground using 2GHz wave band.
Magnetic Sensor for Spacecraft
This sensor measures the magnetic field strength in the space environment, which is necessary for the attitude control of satellite.
Magnetic Torque Actuator for Spacecraft
The magnetic torque actuator is an equipment to control spacecraft attitude due to the effects of the geomagnetic field.
High Voltage Power Supply for Spacecraft
This instrument is a HVPS (high voltage power supply) to be installed on scientific satellite for supplying voltage to detectors in the space environment.
Quartz Crystal Microbalance for Spacecraft
Quartz Crystal Microbalance (QCM) is a unit for monitoring contamination status around satellites by utilizing the characteristics of oscillating frequencies variation depending on the amount of substances attached over the crystal surface.
Particle Detector for Spacecraft
A particle detector instrument observes electron, proton and He. The instrument contributes to investigations into the cause of troubles such as malfunctions of semiconductor devices and electrostatic charge. It also observes the worst environment of trapped particles in the radiation belt, solar flare particles, and auroral particles.
Radiation Ray Monitoring Device
This radiation ray monitoring device (RRMD) measures the high energy cosmic radiation inside the Japanese Experiment Module of the International Space Station in real-time.
Space Station-related Equipment
International Space Station
The experimental module “KIBO” of the International Space Station that has completed in 2009, is the first manned facility that Japan was in charge of development. The IHI group developed the extravehicular experimental platform as well as the extravehicular pallet for “KIBO”, and also developed the experiment racks and experimental devices installed in inboard labs.
Development of a propulsion system and exposed pallet for HTV (H-II Transfer Vehicle).
HTV is a space vehicle which transports supplies and collects waste to/from space stations. The IHI Group develops various satellite propulsion systems, including the HTV propulsion system. Since HTV-1 was launched in 2009, it has been fulfilling its mission, earning a reputation of high reliability and satisfying stringent safety requirements.
Ground Test Facilities
Ground test facility
In addition to the LNG engine firing test facilities, we also possess test facilities for the satellite propulsion systems and control systems.
Sample Containers, etc.
HAYABUSA sample container
Asteroid exploration “HAYABUSA” was launched in 2003 on the M-V rocket No. 5, and the capsule was retrieved from the Woomera Prohibited Area in Australia in 2010. IHI group has the development and manufacturing technologies of the heat resisting materials (CFRP) that can withstand the relentless aerodynamic heating during the atmosphere entry. These materials will be used with the planetary exploration capsules to be produced in future.
Re-entry observation system “i-Ball”
i-Ball is a re-entry data collection device developed by the IHI Group. It is installed on spacecraft, such as HTV, which burn up upon re-entry into the atmosphere. In addition to capturing the nature of destruction upon re-entry, i-Ball measures temperature, acceleration, position and so on using its various sensors. The i-Ball installed on the H-II B-3, launched in September of 2012, has successfully captured images and measured various re-entry data.
Next-generation Unmanned Space Experiment Recovery System (USERS)
USERS is a next-generation unmanned space experiment recovery system which was launched by USEF (currently Japan Space Systems or “JSS”) on the H-IIA-3. The IHI Group designed and developed the re-entry module (REM) and Super Conductor Gradient Heating Furnace (SGHF) as well as oversaw re-entry operations and searched recovery work. In May of 2003, the module was successfully recovered in the Pacific Ocean, east of Ogasawara, making it the first time a spacecraft was recovered from orbit by Japan.
(Source: JSS) (Source: JSS)