Читать книгу Verification of M.Faraday's hypothesis on the gravitational power lines онлайн
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The time of the flight without the inclusion of the propulsion system lasted until June 11, 2009, that is 0,466.108 s. At the point of activation of the brake motor installation altitude was 27.8 km (the distance from the center of 1,776.108 cm), which corresponds to the orbital velocity 1,6661.105 m/s. Then, after 6 minutes the connection with the satellite was lost. Substituting the values of change of orbital parameters in the formula 1, we get the value of the constant C = 2,34.108 cm/s, very close to the values previously calculated for other satellites.
Indian space research organization (ISRO,) reported [10] about the launch of 22 October 2008 on a circumlunar orbit of his device
"Chandrayan-1 using developed in Indian rocket PSLV–XL (PSLV – Polar Satellite Launch Vehicle from Baikonur Satish Dhawan. Starting weight station was 1380 kg, weight station in lunar orbit – 523 kg.
After a series of maneuvers November 4, the station went on the flight path to the Moon and on 8 November reached the environs of the Moon, where at a distance of 500 km from the surface was included brake motor, resulting in the station moved to a transitional circumlunar orbit resettlement 504 km, aposelene 7502 km and an orbital period of 11 hours. Then on 9 November, after adjustment of the pericenter of the orbit was lowered to 200 km. On November 13, the station was transferred to the circular working circumlunar orbit with altitude of 100 km (1,838.108 cm from the center of the Moon), a cycle time of 120 min, the orbital speed 1,6332.105 cm/s.