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DMSP-5D3 F15, 16, 17, 18, 19, 20

DMSP-5D3 [USAF]

DMSP-5D3 (Defense Meteorological Satellite Program Block 5D3) is the eleventh and most recent version of the military meteorological satellites of the Defense Meteorological Satellite Program.

This series introduced a improved version of the DMSP-5D2 3-axis stabilized bus with integrated propulsion system, so that the satellite itself acted as an upper stage for the launch vehicle. It consisted of a single Star-37XFP motor and the ISS (Integrated Stage System) control system featuring four axial hydrazine thrusters. Power was supplied by a single, articulated 8-segmented solar array.

The first two satellites (F15, F16) were launched on Titan-2(23)G rockets and required a Star-37XFP kick motor for orbit insertion. The later satellites (F17 -F20) switched to more powerful EELV class launch vehicles (Atlas-5(401), Delta-4M), which are capable of direct orbit insertion, so the solid fuel kick motor is omitted in these satellites.

Instruments on this series are:

  • OLS (Operational Linescan System) weather imager
  • SSMIS (microwave imager and sounder)
  • SSULI ultraviolet limb imager
  • SSUSI ultraviolet spectrographic imager and nadir airglow photometer
  • SSI/ES-3 thermal plasma instrument
  • SSJ/5 precipitating particle spectrometer
  • SSF laser threat warning sensor

Following instruments are on the individual satellites:

DMSP-5D3 F-15:  OLS, SSM/I, SSJ/4, SSI/ES-2, SSM-Boom, SSZ
DMSP-5D3 F-16:OLS, SSMIS, SSI/ES-3, SSJ5, SSM-Boom, SSULI, SSUSI, SSF
DMSP-5D3 F-17:OLS, SSMIS, SSI/ES-3, SSJ5, SSM-Boom, SSULI, SSUSI, SSF
DMSP-5D3 F-18:OLS, SSMIS, SSI/ES-3, SSJ5, SSM-Boom, SSULI, SSUSI, SSF
DMSP-5D3 F-19:OLS, SSMIS, SSI/ES-3, SSJ5, SSM-Boom, SSULI, SSUSI, SSF
DMSP-5D3 F-20:OLS, SSMIS, SSI/ES-3, SSJ5, SSM-Boom, SSULI, SSUSI, SSF

The DMSP-5D3 series was to be succeded by the jointly with NASA and NOAA developed NPOES system, which was cancelled in 2010 due to massive cost overruns. As a replacement, they were to be replaced by the military DWSS series, which in turn also was cancelled in 2012.

The last satellite, DMSP-5D3 F20, which is in storage since the 1990ies, might eventually not launch, as the Senate drafted a bill, which prohibits the Air Force from spending any money on the DMSP-5D3 F20 launch pending certification from the secretary of defense that the military cannot obtain comparable data at a lower cost from other sources, such as civilian or international weather satellites. In the omnibus spending bill for fiscal year 2016, lawmakers provided no funding neither for DMSP nor for the launch of DMSP-5D3 F-20 around 2018, effectively ending the program.

DMSP-5D3 F19 has stopped responding to commands on 11 February 2016 for reasons unknown. The satellite was recovered to provide tactical data to field units but has not provided full-orbit weather imagery since. It is expected, that the satellite will loose attitude control in September 2019, thus ending the mission. Attitude control was eventually lost in October 2017.

In the aftermath of this failure, the USAF was reconsidering the future of DMSP-5D3 F-20. In late 2016, the USAF began scrapping DMSP-5D3 F-20.

Nation: USA
Type / Application: Meteorology
Operator: US Air Force (USAF) → US Space Force (USSF)
Contractors: Lockheed Martin
Equipment: see above
Configuration: TIROS-N Bus
Propulsion: Star-37XFP / ISS (#15, 16); ISS (17 - 20)
Power: Deployable solar array, batteries
Lifetime: 5 years (design)
Mass: ~1200 kg (#17 - #20)
Orbit: 857 km × 857 km; 99° SSO
Satellite COSPAR Date LS Launch Vehicle Remarks
DMSP-5D3 F15 (DMSP-5D3 S15, USA 147) 1999-067A 12.12.1999 Va SLC-4W Titan-2(23)G Star-37XFP-ISS
DMSP-5D3 F16 (DMSP-5D3 S20, USA 172) 2003-048A 18.10.2003 Va SLC-4W Titan-2(23)G Star-37XFP-ISS
DMSP-5D3 F17 (DMSP-5D3 S17, USA 191) 2006-050A 04.11.2006 Va SLC-6 Delta-4M
DMSP-5D3 F18 (DMSP-5D3 S18, USA 210) 2009-057A 18.10.2009 Va SLC-3E Atlas-5(401)
DMSP-5D3 F19 (DMSP-5D3 S19, USA 249) 2014-015A 03.04.2014 Va SLC-3E Atlas-5(401)
DMSP-5D3 F20 (DMSP-5D3 S16) - not launched Va Atlas-5(401) or Falcon-9 v1.2

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