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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 The J-I was a Solid-fuel rocket expendable launch vehicle developed by the National Space Development Agency of Japan and the Institute of Space and Astronautical Science. In an attempt to reduce development costs, it used the solid rocket boos ...
launcher. It was a successor of
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. OREX tested various communication ...
and was a precursor for the Japanese space shuttle
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 contri ...
. 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 A lifting body is a fixed-wing aircraft or spacecraft configuration in which the body itself produces lift. In contrast to a flying wing, which is a wing with minimal or no conventional fuselage, a lifting body can be thought of as a fuselage wi ...
space plane for gaining technological prowess in the design, production, and flight of
hypersonic In aerodynamics, a hypersonic speed is one that exceeds 5 times the speed of sound, often stated as starting at speeds of Mach 5 and above. The precise Mach number at which a craft can be said to be flying at hypersonic speed varies, since in ...
crafts, as well as technology validation of
atmospheric reentry Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet, or natural satellite. There are two main types of atmospheric entry: ''uncontrolled entry'', such as the entr ...
. The experimental vehicle was covered in carbon–carbon, ceramic tiles, and flexible
thermal insulation Thermal insulation is the reduction of heat transfer (i.e., the transfer of thermal energy between objects of differing temperature) between objects in thermal contact or in range of radiative influence. Thermal insulation can be achieved with s ...
, which were materials that was to be used for HOPE. Launched on 11 February 1996 (UTC) from
Tanegashima Space Center The (TNSC) is the largest rocket-launch complex in Japan with a total area of about 9.7 square kilometers. It is located on the southeast coast of Tanegashima, an island approximately south of Kyushu. It was established in 1969 when the ...
by a
J-I The J-I was a Solid-fuel rocket expendable launch vehicle developed by the National Space Development Agency of Japan and the Institute of Space and Astronautical Science. In an attempt to reduce development costs, it used the solid rocket boos ...
rocket, separation from the rocket was conducted at an altitude of , speed of approximately 3.8 km/s.
Attitude control Attitude control is the process of controlling the orientation of an aerospace vehicle with respect to an inertial frame of reference or another entity such as the celestial sphere, certain fields, and nearby objects, etc. Controlling vehicle ...
was performed by gas thrusters and aerodynamic rudders. During its descent the craft
glided Gliding is a recreational activity and competitive air sport in which pilots fly unpowered aircraft known as gliders or sailplanes using naturally occurring currents of rising air in the atmosphere to remain airborne. The word ''soaring'' is a ...
in a right turn circling the island of
Chichijima , native_name_link = , image_caption = Map of Chichijima, Anijima and Otoutojima , image_size = , pushpin_map = Japan complete , pushpin_label = Chichijima , pushpin_label_position = , pushpin_map_alt = , ...
in the Ogasawara Archipelago. HYFLEX had various sensors attached to each parts, and succeeded in gaining data on surface
aerodynamic heating Aerodynamic heating is the heating of a solid body produced by its high-speed passage through air. In science and engineering, an understanding of aerodynamic heating is necessary for predicting the behaviour of meteoroids which enter the earth's ...
and pressure. The craft splashed down in the waters northeast of Chichijima with
parachute A parachute is a device used to slow the motion of an object through an atmosphere by creating drag or, in a ram-air parachute, aerodynamic lift. A major application is to support people, for recreation or as a safety device for aviators, who ...
s, however the floats and riser broke off while floating and recovery was abandoned. HYFLEX was succeeded by
ALFLEX ALFLEX (Automatic Landing Flight EXperiment) was an experimental unmanned aircraft created by National Space Development Agency of Japan, NASDA and National Aerospace Laboratory of Japan, NAL, the predecessors of JAXA, in 1996. It was built as a ...
.


See also

*
1996 in spaceflight This article outlines notable events occurring in 1996 in spaceflight Spaceflight (or space flight) is an application of astronautics to fly spacecraft into or through outer space, either with or without humans on board. Most spaceflight ...
*
Intermediate eXperimental Vehicle The Intermediate eXperimental Vehicle (IXV) is a European Space Agency (ESA) experimental suborbital re-entry vehicle. It was developed to serve as a prototype lifting body orbital return vehicle to validate the ESA's work in the field of reus ...


References

{{Spaceplanes Satellites of Japan Spaceplanes