Mercury F/O 1 (NROL-67, USA 250) |
USA |
Spacecraft nº: |
US spacecraft nº: |
| Designation | 39652 / 14020A |
| Launch date | 10 April 2014 - 17:45 UT |
| Launch site | CC, SLC-41 |
| Launch vehicle | Atlas-5/541 (AV-045) |
| Mission | ELINT (Sigint) |
| Geosynchronous orbit: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | ° |
| Period | min |
| Prime manufacturer | |
| Platform | |
| Operator | USAF |
| Mass at launch | 3400 - 3850 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | Large Dish Antenna |
| Solar array | |
| Stabilization | 3-Axis-Stabilization |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR696), #14, #228 - update: 02.12.14 | Home |