POLDER explained

POLDER 1
Mission Type:Earth observation
Operator:CNES
Website:CNES Page
Launch Mass:~30kg (70lb)
Power:30W
Launch Rocket:H-II (POLDER 1)
Launch Site:Tanegashima Space Center
Instrument Type:push broom scanner
Telescope Focal Length:3.57mm
Telescope Resolution:242x548 pixels
Trans Band:Formed broad beam pattern UHF antenna
Trans Twta:>5W
Trans Eirp:27.1 dBm
Next Mission:POLDER 2
POLDER 2
Mission Type:Earth observation
Operator:CNES
Website:CNES Page
Launch Mass:~30kg (70lb)
Power:30W
Launch Rocket:H-IIA (POLDER 1)
Launch Site:Tanegashima Space Center
Instrument Type:push broom scanner
Telescope Focal Length:3.57mm
Telescope Resolution:242x548 pixels
Trans Band:Formed broad beam pattern UHF antenna
Trans Twta:>5W
Trans Eirp:27.1 dBm
Previous Mission:POLDER 1
Next Mission:POLDER 3
POLDER 3
Mission Type:Earth observation
Operator:CNES
Website:CNES Page
Launch Mass:~30kg (70lb)
Power:30W
Launch Rocket:Ariane 5G
Launch Site:Guiana Space Centre
Instrument Type:push broom scanner
Telescope Focal Length:3.57mm
Telescope Resolution:242x548 pixels
Trans Band:Formed broad beam pattern UHF antenna
Trans Twta:>5W
Trans Eirp:27.1 dBm
Previous Mission:POLDER 2
Next Mission:PARASOL

POLDER (POLarization and Directionality of the Earth's Reflectances) is a passive optical imaging radiometer and polarimeter instrument developed by the French space agency CNES.

Description

The device was designed to observe solar radiation reflected by Earth's atmosphere, including studies of tropospheric aerosols, sea surface reflectance, bidirectional reflectance distribution function of land surfaces, and the Earth Radiation Budget.

Specifications

POLDER has a mass of approximately 30kg (70lb), and has a power consumption of 77 W in imaging mode (with a mean consumption of 29 W).

Imaging

POLDER utilizes a push broom scanner. The device's optical system uses a telecentric lens and a charged coupled device matrix with a resolution of 242x548 pixels. The focal length is 3.57mm with a focal ratio of 4.6. The field of view ranges from ±43° to ±57°, depending on the tracking method.

Spectral characteristics

The device scans between 443 and 910 nm FWHM, depending on the objective of the measurement. The shorter wavelengths (443–565 nm) typically measure ocean color, whereas the longer wavelengths (670–910 nm) are used to study vegetation and water vapor content.

Data transfer

It transmits data on 465.9875 MHz at bit rate of 200 bit/s, and receives on 401.65 MHz at 400 bit/s. The data rate is 880 kbit/s at a quantization level of 12 bits.

Missions

POLDER was first launched as a passenger instrument aboard ADEOS I on 17 August 1996. The mission ended on 30 June 1997 when communication from the host satellite failed. POLDER 2 was launched in December 2002 aboard ADEOS II. The second mission ended prematurely after 10 months when the satellite's solar panel malfunctioned.A third generation instrument was launched on board the French PARASOL microsatellite. The satellite was maneuvered out of the A-train on 2 December 2009 and permanently shut down on 18 December 2013.[1]

External links

Notes and References

  1. Web site: POLDER/PARASOL Mision. University of Lille. 9 June 2017.