Kakehashi

Launch Partial Failure

Liftoff Time (GMT)

07:55:00

Saturday February 21, 1998

Mission Details

Launch Notes

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.

Kakehashi

Wiki

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.

Geostationary Earth Orbit

1 Payload

3,900 kilograms

Rocket

Retired
H-II

Active 1994 to 1998

Mitsubishi Heavy Industries logo

Agency

MHI

Rocket

Height: 49m

Payload to Orbit

LEO: 10,060 kg

GTO: 3,930 kg

Stages

2

Strap-ons

2

Launch Site

LA-Y1

Tanegashima Space Center, Japan

Fastest Turnaround

25 days 4 hours

Stats

H-II


6th

Mission

1st

Mission of 1998

1998


12th

Orbital launch attempt