TacSat-3

TacSat-3
Artist's rendering of TacSat-3 imaging satellite
NamesJWS-D2
Mission typeTechnology, Communications
OperatorAir Force Research Laboratory (AFRL)
COSPAR ID2009-028A Edit this at Wikidata
SATCAT no.35001
Mission duration2.5 years (planned)
3 years (achieved)
Spacecraft properties
SpacecraftTacSat-3
BusATK
ManufacturerRaytheon
Launch mass400 kg (880 lb)
Start of mission
Launch date19 May 2009, 23:55 UTC
RocketMinotaur I # 8
Launch siteMARS, Wallops Island, LP-0B
ContractorOrbital Sciences Corporation
End of mission
Last contact15 February 2012
Decay date30 April 2012
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeLow Earth orbit
Perigee altitude432 km (268 mi)
Apogee altitude467 km (290 mi)
Inclination40.40°
Period93.57 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]

  1. ^ "Satellite Catalog". Jonathan's Space Report. Retrieved 19 April 2021.
  2. ^ "On-demand intel satellite sensor delivered". United Press International. 12 June 2007. Archived from the original on 4 June 2011.
  3. ^ Kleiman, Michael P. (30 March 2006). "Responsive, flexible, and affordable satellite enhances support to warfighter". afrl.af.mil. Air Force Research Laboratory. Archived from the original on 25 July 2006. Public Domain This article incorporates text from this source, which is in the public domain.