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Launch Overview

Mitsubishi Heavy Industries, Ltd. (MHI) will launch the Japan Aerospace Exploration Agency (JAXA)'s "KIZUNA" (WINDS: Wideband InterNetworking engineering test and Demonstration Satellite) using H-IIA Launch Vehicle No.14 (H-IIA F14) from Tanegashima Space Center.

H-IIA F14

Scheduled Launch
Date
February 23rd (Saturday), 2008
Scheduled Launch Window From 4:20 p.m. to 5:55 p.m. JST
Reserved Launch Period February 24 through 28, 2008
Launch Site Yoshinobu Launch Complex at JAXA's Tanegashima Space Center
KIZUNA Injection Orbit Geostationary Transfer Orbit
Perigee Altitude (km): 250
Apogee Altitude (km): 35,976
Inclination (deg): 28.5
Argument of Perigee (deg): 179
H-IIA/F14(WINDS) Flight Trajectory
H-IIA/F14(WINDS) Flight Timeline

KIZUNA Overview

The Japan Aerospace Exploration Agency (JAXA)'s KIZUNA satellite is responsible for the demonstration of the validity and usefulness of technologies related to large-capacity data communications in our space infrastructure project, "i-Space," the purpose of which is to promote the use of satellites in such fields as Internet communications, education, medicine, disaster measures and Intelligent Transport Systems.
KIZUNA will lead to ultra-high speed international Internet-based communications. The technology takes advantage of the fact that satellite communications are far-reaching, multicasting and disaster-resistant. Ultra-fast satellite-based Internet-based communications will remove the so-called digital divide by providing high-speed Internet service in areas where the terrestrial communications infrastructure is poor. Among other uses, this will make possible great advances in telemedicine, which will bring high-quality medical treatment to remote areas, and in distance education, connecting students and teachers separated by great distances.
More datails (JAXA's website)
KIZUNA image photoKIZUNA image illustration
Courtesy of JAXA


Overview of H-IIA Launch Vehicle No.14 (H-IIA F14)

MHI has prepared an H2A2024 model of the H-IIA launch vehicle equipped with four solid strap-on boosters (SSB) to launch KIZUNA into geostationary transfer orbit. The payload fairing model is 4S (four meters in diameter; dedicated launch fairing).
MHI has applied the LE-5B-2, improved LE-5B liquid rocket engine for the second stage engine to reduce the vibration level for the second stage.
In addition, for the SRB-A solid rocket booster, MHI has applied an improved nozzle and high combustion pressure motor, both verified through the data acquisition tests conducted by JAXA using a full scale model in July, 2006.
H-IIA F14
yH-IIA F14 Specificationz



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