
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 ommited in these satellites.
Instruments on this series are:
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 20xx due to massive cost overruns. As a replacement, they were to be replaced by the military DWSS series, which in turn also was cancelled.
| Nation: | USA |
|---|---|
| Type / Application: | Meteorology |
| Operator: | US Air Force |
| 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: | |
| Mass: | ~1200 kg (#17 - #20) |
| Orbit: | 857 km × 857 km; 99° SSO |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| DMSP-5D3 F15 (DMSP-5D3 S15, USA 147) | 12.12.1999 | Va SLC-4W | Titan-2(23)G Star-37XFP-ISS | ||
| DMSP-5D3 F16 (DMSP-5D3 S20, USA 172) | 18.10.2003 | Va SLC-4W | Titan-2(23)G Star-37XFP-ISS | ||
| DMSP-5D3 F17 (DMSP-5D3 S17, USA 191) | 04.11.2006 | Va SLC-6 | Delta-4M | ||
| DMSP-5D3 F18 (DMSP-5D3 S18, USA 210) | 18.10.2009 | Va SLC-3E | Atlas-5(401) | ||
| DMSP-5D3 F19 (DMSP-5D3 S19) | 2014 | Va SLC-3E | Atlas-5(401) | ||
| DMSP-5D3 F20 (DMSP-5D3 S16) | 2020 | Va SLC-6 | Delta-4M |