AEHF 6 (USA 298) |
USA |
Int. spacecraft nº: |
US spacecraft nº: |
Launch data:
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| Prime manufacturer | Lockheed Martin (Bus), Northrop Grumman (ex TRW) (Payload) |
| Platform | A2100M |
| Operator | US Air Force (USAF) ? US Space Force (USSF) |
| Mass at launch | 6168 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | 2 deployable 5 segment solar arrays |
| Stabilization | |
| Propulsion | IHI BT-4, 4 × XR-5 Hall Current Thrusters |
| DC power | |
| Design lifetime | 14 yrs |
| Ref.: #7(JR777), #14 - update: 01.05.20 | Home |