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OREX
OREX (Orbital Re-entry Experiment) was a NASDA re-entry demonstrator prototype which was launched in 1994 on the H-II launcher; the satellite was renamed . It was a precursor for the Japanese space shuttle HOPE Hope is an optimistic state of mind that is based on an expectation of positive outcomes with respect to events and circumstances in one's own life, or the world at large. As a verb, Merriam-Webster defines ''hope'' as "to expect with confid .... OREX tested various communications systems, heating profiles and heat shielding components for HOPE. See also * ALFLEX * HOPE-X * HYFLEX References External links Description of OREX on JAXA web site Satellites of Japan Spacecraft launched in 1994 {{Japan-spacecraft-stub ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
H-II
The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues. Background Prior to H-II, NASDA had to use components licensed by the United States in its rockets. In particular, crucial technologies of H-I and its predecessors were from the Delta rockets (the manufacturer of the Delta rockets, McDonnell Douglas, later Boeing and the United Launch Alliance, would later use the H-IIA's technologies (the rocket itself is the successor to the H-II) to create the Delta III, albeit short lived). Although the H-I did have some domestically produced components, such as LE-5 engine on the second stage and inertial guidance system, th ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Yoshinobu Launch Complex
Yoshinobu Launch Complex (abbreviated as LA-Y) is a List of rocket launch sites, rocket launch site at the Tanegashima Space Center on Tanegashima. The site and its collection of facilities were originally built for the H-II launch vehicle and later used for H-IIA, H-IIB and H3 (rocket), H3 launches. It is the most Northern launch complex at Tanegashima, and along with the now inactive Osaki Launch Complex used for orbital launches. The Yoshinobu Launch Complex consists of two launch pads. The complex also contains a Engine test stand, test stand for firing the LE-7 engines used in the first stage of the H-II and its derivatives. Prior to launch, rockets are processed vertically in the complex's vehicle assembly building. The rocket is rolled out to the launch pad on a mobile launcher platform about twelve hours before it is scheduled to launch. It takes around thirty minutes to transport the rocket from the assembly building to Pad 1. See also * References Space ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
HOPE-X
HOPE (H-II Orbiting Plane) was a Japanese experimental spaceplane project designed by a partnership between NASDA and NAL (both now part of JAXA), started in the 1980s. It was positioned for most of its lifetime as one of the main Japanese contributions to the International Space Station, the other being the Japanese Experiment Module. The project was eventually cancelled in 2003, by which point test flights of a sub-scale testbed had flown successfully. History At the time of the planning phase for HOPE-X, Japanese spaceflight had seen a string of successful advancements in the decade prior, including the development of the N-I and N-II rocket systems and the launch of the first Japanese satellites. Japan was a participant in plans for the Space Shuttle program as well as the proposed Space Station Freedom (later the ISS), and sought development of a vehicle to support its cooperation with the United States in low Earth orbit operations. By 1990, NASDA had established the ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
ALFLEX
ALFLEX (Automatic Landing Flight EXperiment) was an experimental unmanned aircraft created by NASDA and NAL, the predecessors of JAXA, in 1996. It was built as a successor to HYFLEX as part of the HOPE program. ALFLEX was built to establish the basic technology of automatic landing. The design featured a streamlined metal hull, delta planiform wings, and large winglets. Despite being a project of Japanese aerospace agencies, ALFLEX never left the atmosphere. Instead, it was carried up to a high altitude by a helicopter, then released to automatically glide down to the designated landing site, navigating by means of onboard computers. ALFLEX completed thirteen drop tests from July to August 1996, all of which were successful. Specifications (ALFLEX) * Length (without pitot boom): 6.10 m * Wingspan: 3.78 m * Height (without gear): 1.35 m See also * HOPE-X * HYFLEX * OREX OREX (Orbital Re-entry Experiment) was a NASDA re-entry demonstrator prototype which was launched in 1 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
HYFLEX
HYFLEX (Hypersonic Flight Experiment) was a National Space Development Agency of Japan reentry demonstrator prototype which was launched in 1996 on the only flight of the J-I launcher. It was a successor of OREX and was a precursor for the Japanese space shuttle HOPE-X. HYFLEX tested the carbon-carbon heat shielding tiles that were intended to be used on HOPE, as well as having the same body shaping in order to gather data on hypersonic lifting. HYFLEX flew in space at altitude and succeeded in re-entry, but sank in the Pacific after splashdown before it could be recovered. Overview HYFLEX was an uncrewed lifting body space plane for gaining technological prowess in the design, production, and flight of hypersonic crafts, as well as technology validation of atmospheric reentry. The experimental vehicle was covered in carbon–carbon, ceramic tiles, and flexible thermal insulation, which were materials that was to be used for HOPE. Launched on 11 February 1996 (UTC) from ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Kakamigahara Air And Space Museum
Gifu-Kakamigahara Air and Space Museum is an aviation museum located in Kakamigahara in Gifu Prefecture in Japan. It is at Gifu Air Field of the Japan Air Self-Defense Force. Overview The museum features outdoor and indoor exhibits, featuring aviation and space displays about the history and stories on the development of aviation technology, and information on the latest space technology. Named originally Kakamigahara Aerospace Museum and later Kakamigahara Aerospace Science Museum. it was jointly established by Kakamigahara City and Gifu Prefecture and renamed Gifu-Kakamigahara Aerospace Museum after extensive renovation in 2018. Aircraft on display Outdoor Exhibits * Kawasaki V-107 * NAMC YS-11 * ShinMeiwa US-1A Indoor Exhibits * Wright Flyer (replica) * Grade monoplane (replica) * Salmson 2 (replica) * Mitsubishi A6M Zero (replica) * Kawasaki Ki-61 (the sole surviving aircraft of this type) * Kawasaki KAL-1 * Kawasaki KAT-1 * Lockheed T-33 * SAAB X1G * Fuji ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
NASDA
The , or NASDA, was a Japanese national space agency established on October 1, 1969 under the National Space Development Agency Law only for peaceful purposes. Based on the Space Development Program enacted by the Minister of Education, Culture, Sports, Science and Technology (MEXT), NASDA was responsible for developing satellites and launch vehicles as well as launching and tracking them. The first launch vehicles of NASDA ( N-I, N-II, and H-I) were partially based on licensed technology from the United States, particularly the Delta rocket family. The H-II was the first liquid fuel rocket to be fully developed in Japan. Hideo Shima, chief engineer of the original Shinkansen "bullet train" project, served as Chief of NASDA from 1969 to 1977. On October 1, 2003, NASDA merged with the Institute of Space and Astronautical Science (ISAS) and the National Aerospace Laboratory of Japan (NAL) into one Independent Administrative Institution: the Japan Aerospace Exploration A ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Tanegashima Space Center
The (TNSC) is Japan's primary spaceport, covering approximately about . It is located on the southeastern tip of Tanegashima, the easternmost of the Ōsumi Islands, approximately south of the major island of Kyushu. The site was selected on May 24, 1966, and construction began later that year on September 17. Exactly two years later, on September 17, 1968, it hosted its first launch, a small rocket. The facility officially opened on October 1, 1969, coinciding with the establishment of its initial operator, the National Space Development Agency of Japan (NASDA). Now operated by the Japan Aerospace Exploration Agency The is the Japanese national Aeronautics, air and space agency. Through the merger of three previously independent organizations, JAXA was formed on 1 October 2003. JAXA is responsible for research, technology development and launch of satell ... (JAXA) since its formation in 2003, TNSC is responsible for satellite assembly, as well as launch vehicle test ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Pacific Ocean
The Pacific Ocean is the largest and deepest of Earth's five Borders of the oceans, oceanic divisions. It extends from the Arctic Ocean in the north to the Southern Ocean, or, depending on the definition, to Antarctica in the south, and is bounded by the continents of Asia and Australia in the west and the Americas in the east. At in area (as defined with a southern Antarctic border), the Pacific Ocean is the largest division of the World Ocean and the hydrosphere and covers approximately 46% of Earth's water surface and about 32% of the planet's total surface area, larger than its entire land area ().Pacific Ocean . ''Encyclopædia Britannica, Britannica Concise.'' 2008: Encyclopædia Britannica, Inc. The centers of both the Land and water hemispheres, water hemisphere and the Western Hemisphere, as well as the Pole of inaccessi ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Geocentric Orbit
A geocentric orbit, Earth-centered orbit, or Earth orbit involves any object orbiting Earth, such as the Moon or artificial satellites. In 1997, NASA estimated there were approximately 2,465 artificial satellite payloads orbiting Earth and 6,216 pieces of space debris as tracked by the Goddard Space Flight Center. More than 16,291 objects previously launched have undergone orbital decay and entered Earth's atmosphere. A spacecraft enters orbit when its centripetal acceleration due to gravity is less than or equal to the centrifugal acceleration due to the horizontal component of its velocity. For a low Earth orbit, this velocity is about ; by contrast, the fastest crewed airplane speed ever achieved (excluding speeds achieved by deorbiting spacecraft) was in 1967 by the North American X-15. The energy required to reach Earth orbital velocity at an altitude of is about 36 MJ/kg, which is six times the energy needed merely to climb to the corresponding altitude. Spa ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Low Earth Orbit
A low Earth orbit (LEO) is an geocentric orbit, orbit around Earth with a orbital period, period of 128 minutes or less (making at least 11.25 orbits per day) and an orbital eccentricity, eccentricity less than 0.25. Most of the artificial objects in outer space are in LEO, peaking in number at an altitude around , while the farthest in LEO, before medium Earth orbit (MEO), have an altitude of 2,000 km, about one-third of the Earth radius, radius of Earth and near the beginning of the Van Allen radiation belt#Inner belt, inner Van Allen radiation belt. The term ''LEO region'' is used for the area of space below an altitude of (about one-third of Earth's radius). Objects in orbits that pass through this zone, even if they have an apogee further out or are sub-orbital spaceflight, sub-orbital, are carefully tracked since they present a collision risk to the many LEO satellites. No human spaceflights other than the lunar missions of the Apollo program (1968-1972) have gone beyond L ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
National Space Development Agency Of Japan
The , or NASDA, was a Japanese national space agency established on October 1, 1969 under the National Space Development Agency Law only for peaceful purposes. Based on the Space Development Program enacted by the Minister of Education, Culture, Sports, Science and Technology (MEXT), NASDA was responsible for developing satellites and launch vehicles as well as launching and tracking them. The first launch vehicles of NASDA ( N-I, N-II, and H-I) were partially based on licensed technology from the United States, particularly the Delta rocket family. The H-II was the first liquid fuel rocket to be fully developed in Japan. Hideo Shima, chief engineer of the original Shinkansen "bullet train" project, served as Chief of NASDA from 1969 to 1977. On October 1, 2003, NASDA merged with the Institute of Space and Astronautical Science (ISAS) and the National Aerospace Laboratory of Japan (NAL) into one Independent Administrative Institution: the Japan Aerospace Exploration Agen ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
