Official name AEHF 2 (USA 235)
Alternative name USA 235
Cospar ID 2012-019A
Norad ID 38254
Launch date 2012-05-04
Launch site AFETR
Launch vehicle Atlas-5(531)¹
Country/Organization USA
Type application Comsat
Operator US Air Force (USAF) → US Space Force (USSF)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.07
Inclination (deg) 5.75
Perigee (km) 35774
Apogee (km) 35798
Eccentricity 0.00033532666405857
Mean motion (revs. per day) 1.00273663540078
Semi-Major axis (km) 42164.135
Raan (deg) 60.0827
Arg of perigee (deg) 10.4159
Shape Box + 2 Pan
Mass (kg) 6200
Height (m) 9.8
Width (m) 2
Depth (m) 2
Span (m^2) 27
Lifetime 14 years
Contractors Lockheed Martin (Bus), Northrop Grumman (ex TRW) (Payload)
Equipment ?
Propulsion IHI BT-4, 4 × XR-5 Hall Current Thrusters
Configuration A2100M
Power 2 deployable 5 segment solar arrays, batteries

The AEHF (Advanced Extreme High Frequency Satellite), a.k.a. AWS (Advanced Wideband Satellite), program is the next generation of highly secure, high capacity, survivable communications to the U.S. warfighters during all levels of conflict, and will become the protected backbone of the Department of Defense's military satellite communications architecture.

The AEHF system will be integrated into the legacy Milstar (Military Strategic & Tactical Relay) constellation, and will be backward compatible with Milstar's low data rate (LDR) and medium data rate (MDR) capabilities, while providing extreme data rates (XDR) and larger capacity at substantially less cost than the Milstar system. Each satellite will be launched on an Evolved Expendable Launch Vehicle (EELV), with the first launch originally planned for April 2008. The first launch was delayed until 2010. They cost approximately $580 million per satellite.

On-board signal processing will provide protection and ensure optimum resource utilization and system flexibility among the Armed Forces and other users who operate terminals on land, sea and air. The AEHF system will be integrated into the legacy Milstar constellation, and will be backward compatible with Milstar's low data rate (LDR) and medium data rate (MDR) capabilities, while providing extreme data rates (XDR) and larger capacity at substantially less cost than the Milstar system.

AEHF satellites feature following antennas:

  • 2 SHF Downlink Phased Arrays,
  • 2 Crosslinks,
  • 2 Uplink/Downlink Nulling Antennas,
  • 1 Uplink EHF Phased Array,
  • 6 Uplink/Downlink gimbaled Dish Antenna,
  • 1 Each Uplink/downlink earth coverage horns

Up to six satellites were planned, but in late 2004 it was decided, to end the AEHF program after the third satellite in favour of introducing the next generation T-Sat earlier. Problems with the T-Sat program led to procurement of two more AEHFs instead. Later a sixth was added.

AEHF 1 was launched in August 2010. After launch, the apogee propulsion system developed problems and the orbit was raised over a longer period using the attitude control engines and the Hall Current Thruster electric propulsion system consisting of four XR-5 5 kW Hall thrusters.

Satellite COSPAR Date LS Launch Vehicle Remarks
AEHF 1 (USA 214) 2010-039A 2010-08-14 AFETR Atlas-5(531)¹
AEHF 2 (USA 235) 2012-019A 2012-05-04 AFETR Atlas-5(531)¹
AEHF 3 (USA 246) 2013-050A 2013-09-18 AFETR Atlas-5(531)¹
AEHF 4 (USA 288) 2018-079A 2018-10-17 AFETR Atlas-5(551)¹
AEHF 5 (USA 292) 2019-051A 2019-08-08 AFETR Atlas-5(551)¹ with TDO 1
AEHF 6 (USA 298) 2020-022B 2020-03-26 AFETR Atlas-5(551)¹ with TDO 2