SATELLITES-------
ATS-ATS VI--------
ATS-ATS VI--------
SPACECRAFT DESCRIPTION:
The spacecraft was a cylinder 56 inches in diameter, 57 inches high and weighed 750 pounds. A phased array of eight whip antennas extended from the top, and a phased array of eight VHF antennas extended from the base. The sides of the cylinder were covered by 23,870 solar cells which, along with nicad batteries, provided the power for the craft. Two meteorological experiments were on board. One was a spin scan cloud camera which provided continuous, full-disk hemispheric images of the sun-lit Earth every half hour. The spinning motion of the satellite generated line scans with a spatial resolution of 3.2 kilometers. This process took approximately twenty minutes for the full image, and then ten minutes to reset the camera for a new image. The second experiment was Weather Facsimile (WEFAX), a data relay and re-transmission instrument. This instrument relayed data from the central ESSA data processing facility to APT ground stations located around the western hemisphere.
The spacecraft was a cylinder 56 inches in diameter, 57 inches high and weighed 750 pounds. A phased array of eight whip antennas extended from the top, and a phased array of eight VHF antennas extended from the base. The sides of the cylinder were covered by 23,870 solar cells which, along with nicad batteries, provided the power for the craft. Two meteorological experiments were on board. One was a spin scan cloud camera which provided continuous, full-disk hemispheric images of the sun-lit Earth every half hour. The spinning motion of the satellite generated line scans with a spatial resolution of 3.2 kilometers. This process took approximately twenty minutes for the full image, and then ten minutes to reset the camera for a new image. The second experiment was Weather Facsimile (WEFAX), a data relay and re-transmission instrument. This instrument relayed data from the central ESSA data processing facility to APT ground stations located around the western hemisphere.
|
||
|
||