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Television InfraRed Observation Satellite (TIROS) is a series of early weather satellites launched by the United States, beginning with TIROS-1 in 1960. TIROS was the first satellite that was capable of remote sensing of the Earth, enabling scientists to view the Earth from a new perspective: space. [1]
TIROS-9 was a spin-stabilized meteorological spacecraft designed to test experimental television techniques and infrared equipment. The satellite was in the form of an 18-sided right prism, 107 cm in diameter and 56 cm high. The top and sides of the spacecraft were covered with approximately 9000 1-by 2-cm silicon solar cells.
The TIROS-1 magnetic tape data recorder.. TIROS 1 was an 18-sided right prism, 107 centimetres (42 in) across opposite corners and 56 centimetres (22 in) high.. Spacecraft power was supplied by approximately 9000 1 centimetre (0.39 in)- by 2 centimetres (0.79 in) silicon solar cells mounted on the cover assembly and by 21 nickel-cadmium batteries.
Pages in category "Television Infrared Observation Satellites" The following 44 pages are in this category, out of 44 total. This list may not reflect recent changes .
The satellite was in the form of an 18-sided right prism, 107 cm in diameter and 56 cm high. The top and sides of the spacecraft were covered with approximately 9000 1- by 2-cm silicon solar cells. TIROS-3 was equipped with two independent television camera subsystems for taking cloud cover pictures, plus a two-channel low-resolution radiometer ...
The flight control system also optimized the performance of the solar cells and TV cameras and protected the five-channel infrared radiometer from prolonged exposure to direct sunlight. TIROS-8 was the first satellite to be equipped with Automatic Picture Transmission (APT) capabilities. The APT experiment provided real-time earth-cloud ...
TIROS-2 was an 18-sided right prism, 107 cm in diameter and 56 cm high, [2] with 9,260 [1] 1 by 2 cm silicon solar cells covered the top and sides. Five small directly opposed pairs of solid-fuel thrusters maintained a spin of 8 to 12 rpm. [2]
TIROS 6 was designed to further demonstrate the capability of a spacecraft to observe, record, and transmit TV cloud cover pictures for use in operational weather analysis and forecasting. The spin-stabilized satellite was in the form of an 18-sided right prism, 107 cm across opposite corners and 56 cm high, with a reinforced baseplate carrying ...
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