It was designed to meet diverse launch demands, at lower cost and with a high
degree of reliability. H-IIA has a simplified design and uses improved
efficiency in the manufacturing and launch processes than its predecessor the
H-II. The first experimental flight of the H-IIA F1 was launched in August 2001.
The Japan Aerospace Exploration Agency has four types of standard launch
vehicles for different weights of payloads. In the case of H-IIA Launch Vehicle
No.1 (H-IIA F1), it was four meters in diameter and 53 meters in height.
Japan may resume launches of the H2A satellite launcher in February 2005 carrying MTSAT. This is the first flight since the last H2A failure in November 2003.
H-IIA Links:
H-IIA Launch Vehicle | JAXA:Goto Rockets (Expendable) Home Page
Goto Space Projects and Info Home Page
Copyright © 2000-2008 Vic Stathopoulos. All rights reserved.
Updated: Saturday 5th, July, 2008