The H-IIA vehicle is an upgraded version of the H-II currently in
service. The H-IIA is intended to compete comercially on the world market. In
1997, Hughes signed a contract for 10 H-IIA launches valued at approximately US$1
billion. The H-IIA builds upon it's predecessor and incorporates a simplified design
and manufacturing process as well as upgraded avionics and engines (LE-7A and
LE-5B). Although the core vehicle is very similar to the H-II, the new H-IIA uses
new solid and liquid boosters to significantly improve payload performance.

The H-IIA comes in five
variants. The basic H2A202 configuration uses a core vehicle with two Solid Rocket
Boosters (SRB-A's) to place four metric tons into a 28.5 degree GTO orbit. The
H2A2022 and H2A2024 configurations add two and four Solid Strap-On Boosters (SSB's)
respectively to increase GTO performance up to 4.5 metric tons. Adding Liquid
Strap-On Boosters (LRB's) to the basic H2A202 configuration creates the H2A212 (one LRB)
and H2A222 (two LRB's) configurations which are capable of placing 7.5 and 9.5 metric tons
into a GTO orbit.

| Prime Contractor: |
National Space Development
Agency of Japan (NASDA) |
| Point of Contact |
NASDA Office of Space
Transportation System
Hamamatsu-cho World Trade Center Building 26F
2-4-1 Hamamatsu-cho, Minato-ku Tokyo, 108-8060 Japan
Tel: + 81.3.3438.6465
Fax: + 81.3.5402.6527 |
| Launch Site: |
Tanegashima Space
Center, Japan
(30.2 deg. N Latitude) |
| Web Links: |
H-IIA Web Site |
|