About Experimental Communications Satellites "Ayame" (ECS)
|
These satellites were launched with the objective of conducting millimeter wave experiments with a satellite. However, the Ayame(ECS) was unable to accomplish its mission, mainly because the 3rd stage rocket came in contact with the satellite after separation. Then the auxiliary Ayame-2(ECS-b) was launched, and it stopped transmitting soon after the apogee engine fired. We learned some valuable lessons on satellite separation technology and apogee engine from this experience. |
|---|
Major Characteristics
| Ayame (ECS) |
International Designation Code | 1979-009A |
|---|---|---|
| Launch Date | 2/6/1979 | |
| Launch Vehicle | N-I Launch Vehicle (N5F) | |
| Launch Site | Tanegashima Space Center | |
| Ayame-2 (ECS-b) |
International Designation Code | 1980-018A |
| Launch Date | 2/22/1980 | |
| Launch Vehicle | N-I Launch Vehicle (N6F) | |
| Launch Site | Tanegashima Space Center | |
| Weight | 130kg | |
| Dimensions | Cylindrical D:141cm | |
| Attitude Control | Spin-stabilized | |