
KIKU-5(ETS-V) was launched to confirm H-I (3-stage) launch vehicle performance, as well as to establish basic geostationary three-axis bus system technology for future satellite applications, amass independent technology required for next-generation satellite development and carry out experiments for mobile communications satellite.
KIKU-5 finished its 1.5 year programmed opration on March 31,1989,while AMEX(Aerouautical Mobile. Experimeutal Trauspouder)still keeps gathering data and carring out experments.
| Launch Date | 8/27/1987 |
|---|---|
| Launch Vehicle | H-I Launch Vehicle(H17F) |
| Launch Site | Tanegashima Space Center |
| Weight | 550kg |
| Orbit | Geostationary 150deg. E. longitude |
| Dimensions | Box shaped with attached deployable solar panels |
| Mission Life | 1.5 years |
| Attitude Control | Three-axis stabilized |