The NOAA K, L and M POES satellites begin the fifth generation of improved
environmental monitoring in support of NOAA missions. The instrument payload has
significant improvements and additions/deletions. The instrument changes have effected the
spacecraft subsystems and data formats.
The NOAA KLM satellites include improvements to instruments that are evolutionary and
significant. The initial concept was to add more passive microwave instruments and
channels in place of the four channel Microwave Sounding Unit (MSU) and the three channel
Stratospheric Sounding Unit (SSU). During the satellite system design process, it became
evident that the increased size, fields of view, and power requirements for the new
instruments would have significant impacts on the spacecraft power, data handling, and
attitude control systems.
Following instruments were carried on board:
- AVHRR/3 (advanced very high resolution radiometer Version 3) for observing daytime and nighttime global cloud cover
- ATOVS (Advanced TIROS operational vertical sounder) suite, for obtaining temperature and water-vapor profiles through the earth's atmosphere. It consists of
- HIRS/3 (High Resolution Infrared Radiation Sounder Version 3)
- AMSU-A (Microwave Sounding Unit A)
- AMSU-B (Microwave Sounding Unit B)
- SEM-2 (Space environment monitor), which measured the proton and electron fluxes near the earth
- Argos-2 (DCS-2)
- S&RSAT
The NOAA KLM spacecraft are significantly heavier than previous spacecraft (2231.7 kg versus 1712.3 kg) and require a more powerful Apogee Kick Motor (AKM) solid rocket booster and expendable launch vehicle, Titan-2(23)G Star-37XFP-ISS, to obtain orbit.
Combined with command system security and frequency changes, NOAA KLM satellites look
very much like previous satellites to the casual observer, but have significant changes to
essentially every subsystem. To meet the increased power requirements, two additional
solar panels have been added and the solar array has about 45% more output. The batteries,
propulsion tank capacity, the size of the reaction wheels and magnetic coils used for
momentum unloading and attitude control have also increased in capacity. The spacecraft
structure has been stiffened primarily to support the heavier AMSU instruments and improve
launch vehicle load margins. Several antennas have been relocated and/or built with new
materials and processes to improve performance. Flight computer memory has been doubled
and the flight software modified to meet new requirements.
NOAA 16 was decommissioned 9 June 2014 after a critical anomaly. On 23 November 2015, it apparently suffered a break-up event. NOAA 17 was decomissioned on 10 April 2013. On 10 March 2021 it also suffered a break-up event.
.png)
