Mercury F/O 1 (NROL-67, USA 250)

USA

Spacecraft nº:

US spacecraft nº:


Launch data:

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


Spacecraft data:

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  


Mission details:

External links:


Ref.: #7(JR696), #14, #228 - update: 02.12.14 Home