FalconSat 8 (FS 8 - USA 300) |
USA |
Int. spacecraft nº: |
US spacecraft nº: |
| Designation | 45610 / 20029B |
| Launch date | 17 May 2020 |
| Launch site | CC, SLC-41 |
| Launch vehicle | Atlas-V (501) |
| Mission | Experimental |
| Launch platform | OTV 6, LEO |
| Deployment date | 28? May 2020 |
| Earth orbit: | |
| Perigee / Apogee | 389 x 389 km |
| Inclination | 45.0° |
| Period | min |
| Prime manufacturer | U.S. Air Force Academy |
| Platform | |
| Operator | U.S. Air Force Academy |
| Mass at launch | 136 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | MEP, MMA, CANOE, ACES, SkyPad |
| Solar array | Solar cells |
| Stabilization | |
| Propulsion | Magnetogradient Electrostatic Plasma Truster |
| DC power | |
| Design lifetime |
| Ref.: #7(JR778-779) - update: 16.06.20 | Home |