NEXT SPACEFLIGHT

Status

Partial Failure

Kakehashi

Launch Time
Sat Feb 21, 1998 07:55 UTC

Last flight of H-II. Faulty brazing in second-stage engine cooling system caused engine burn through and cable damage resulting in shutdown midway through the upper stage's second burn, leaving spacecraft in elliptical LEO instead of GTO. Spacecraft thrusters raised orbit enough to complete some communications experiments.

Rocket

H-II
MHI
Status: Retired
Payload to LEO: 10,060 kg
Payload to GTO: 3,930 kg
Stages: 2
Strap-ons: 2
Rocket Height: 49.0 m

Mission Details

Kakehashi

COMETS (Communication Engineering Test Satellite) a two-ton geostationary three-axis stabilized satellite, is being created to develop the new technologies required for future fields in communications and broadcasting.

Relay satellites in geostationary orbit will be used to develop the following technologies:

- Inter-orbit communications technology for relay of communications between observation satellites or space stations in low-altitude circular orbits and earth stations.
- Advanced satellite broadcast technology for broad-band region-specific broadcasts and high definition television broadcasts using K-band frequency bands.
- Development of advanced mobile satellite communications technology possessing reproduction relay and inter-beam connection functions by employing K-bands and miliband frequencies.

Payloads: 1
Total Mass: 3,900.0 kg
Geostationary Earth Orbit

Location

LA-Y1, Tanegashima Space Center, Japan

Stats

1998

12th orbital launch attempt

H-II

6th mission
1st mission of 1998