Amos 6 |
Israel |
Int. spacecraft nº: |
Israel spacecraft nº: |
| Designation | 16E01 |
| Launch date | 01 Sep 2016 |
| Launch site | CC, SLC-40 |
| Launch vehicle | Falcon-9 v1.2 |
| Mission | Communication |
| Decay | 01 Sep 2016 |
| Prime manufacturer | IAI (prime); MDA (payload) |
| Platform | AMOS-HP bus |
| Operator | Spaxecom Ltd. |
| Mass at launch | 5250 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | 39 Ku-band transponders, 24 Ka-band spot beams, 2 S-band transponders |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | S400 |
| DC power | |
| Design lifetime | 16 yrs |
| Ref.: #14 - update: 08.01.17 | Home |