Results of observations of the radiation environment of a satellite in a semisynchronous orbit during the period from 1965 to 1971

Physics

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Aerospace Environments, Radiation Dosage, Satellite Orbits, Synchronous Satellites, Gas Discharge Tubes, Ionization Chambers, Molniya Satellites, Radiation Counters

Scientific paper

The penetrating radiation along the path of the Molniia-1 satellite was systematically measured during a period of roughly 6 years. The satellite had an apogee of 40,000 km, a perigee of 500 km, an orbital inclination of 65 degrees, and a circling time of 11 hr 57 min. Measurements were carried out with IK-4 ionization chambers and SI-3BG gas-discharge counters. The results, presented in the form of graphs, are suitable for testing the accuracy of the method of trajectory coefficients in predicting the radiation dose on spacecraft elements.

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