Names | JWS-D2 |
---|---|
Mission type | Technology, Communications |
Operator | Air Force Research Laboratory (AFRL) |
COSPAR ID | 2009-028A |
SATCAT no. | 35001 |
Mission duration | 2.5 years (planned) 3 years (achieved) |
Spacecraft properties | |
Spacecraft | TacSat-3 |
Bus | ATK |
Manufacturer | Raytheon |
Launch mass | 400 kg (880 lb) |
Start of mission | |
Launch date | 19 May 2009, 23:55 UTC |
Rocket | Minotaur I # 8 |
Launch site | MARS, Wallops Island, LP-0B |
Contractor | Orbital Sciences Corporation |
End of mission | |
Last contact | 15 February 2012 |
Decay date | 30 April 2012 |
Orbital parameters | |
Reference system | Geocentric orbit[1] |
Regime | Low Earth orbit |
Perigee altitude | 432 km (268 mi) |
Apogee altitude | 467 km (290 mi) |
Inclination | 40.40° |
Period | 93.57 minutes |
TacSat-3 patch mission |
TacSat-3 is the second in a series of U.S. military experimental technology and communication satellites. It was assembled in an Air Force Research Laboratory (AFRL) Space Vehicles Directorate facility at Kirtland Air Force Base, New Mexico.[2] The TacSat satellites are all designed to demonstrate the ability to provide real-time data collected from space to combatant commanders in the field.
TacSat-3 includes three distinct payloads:[3]