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DFH-1
DFH-1
DFH-1
Credit: via Sven Grahn
Chinese communications technology satellite. First Chinese satellite. The initial satellite was flown for purely propaganda purposes, using a tune generator to play the 'East is Red'. Technology satellite for Chinese Academy of Space Technology (CAST), China. Launched 1970.

AKA: Mao;Shi Jian. Status: Operational 1969. First Launch: 1969-11-16. Last Launch: 1971-03-03. Number: 3 . Gross mass: 173 kg (381 lb). Height: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft).

The second included a magnetometer and cosmic/x-ray detectors in place tune generator.

In 1958 the Chinese Academy of Sciences formed a small task group, code named 581, headed by Tsien Hsue-Shen (Qian Xuesen) and Zhao Jiuzhang, to design China's first satellite. In 1965 the State Council reviewed the draft 'Plan for the Development of China's Artificial Satellites'. The evaluation group, code named 651, discussed the objectives and operational tasks of the DFH-1 (Dongfanghong, East is Red) satellite. The DFH-1 would be a scientific test satellite and include transmission of radio signals. Research and development of the satellite and its CZ-1 launch rocket began in November 1966. The planned schedule was severely disrupted by the Cultural Revolution. The DFH-1 as originally designed would have a mass of 150 kg. The last stage of the booster was equipped with an 'observation skirt' that would deploy to increase its reflectivity.

In 1968, the Chinese Academy of Space Technology (CAST) was established and put in charge of realizing the DFH-1. It was orbited as the first Chinese artificial satellite on 24 April 1970. The satellite was composed of seven subsystems - structure, thermal control, power supply, 'The East Is Red' tune generating device, short wave telemetry, tracking and radio, and attitude measurement. The total mass of the spin stabilized satellite was 173 kg. Its shape was similar to the American Telstar, a seventy-two-face polyhedron 1 m in diameter. The satellite was spin stabilized during its flight in space. Min Guiyong headed the development staff at CAST in qualifying the satellite for space flight, including thermal vacuum simulation tests.

After reaching orbit, the satellite drew power from on-board batteries and began broadcasting the 'East is Red' Chinese national anthem at 20.009 MHz. DFH-1 had a design life of 15 days. Other systems functioned nominally and recorded some physics measurements. The third stage of CZ-1 had an "observation skirt" mounted to increase its reflectivity to magnitude 2 to 3. The brightness of the DFH-1 itself was much fainter, ranging from magnitude 5 to 8. At its brightest, DFH-1 was barely visible to the naked eye from a very dark location. At its faintest, the satellite was beyond the threshold of naked eye visibility. The primary purpose of the satellite was to conduct tests of communications satellite technology.

On 3 March, 1971, the second DFH-1, designated SJ-1 (Practice-1) satellite was launched. The design life of the satellite was one year, but it operated in space for more than 8 years until its decay on 11 June, 1979. During the entire period the solar power supply system, thermal control system and long-term telemetry system continued to function. The second DFH was 48 kg heavier, covered with solar cells, and was able to continuously transmit data at 19.995 MHz. It included a magnetometer and cosmic/x-ray detectors in place of the 'East is Red' tune generator on the first DFH.


More at: DFH-1.

Family: Communications technology sat, Technology. Country: China. Launch Vehicles: DF-3, Chang Zheng 1. Launch Sites: Jiuquan, Jiuquan LA2A. Agency: MAI, CAST, CASC. Bibliography: 2, 434, 5, 532, 534, 6, 12206.
Photo Gallery

DFH-1DFH-1
Credit: © Mark Wade


DFH-1DFH-1
Credit: © Mark Wade


DFH-1DFH-1
Credit: © Mark Wade


DFH-1 in OrbitDFH-1 in Orbit


DFH-1 - people's joyDFH-1 - people's joy


DFH-1 in ShroudDFH-1 in Shroud


DFH-1 ReflectorDFH-1 Reflector


DFH-1 solar reflectoDFH-1 solar reflecto


DFH-1 in ShroudDFH-1 in Shroud


DFH-1 in ShroudDFH-1 in Shroud


DFH-1 in ShroudDFH-1 in Shroud


DFH-1 ReflectorDFH-1 Reflector


DFH Mao 1DFH Mao 1
Credit: Manufacturer Image


SJ-1SJ-1
Credit: Manufacturer Image



During 1962 - .
January 1965 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1965 April 29 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1965 August 10 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
May 1966 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1967 January 23 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1968 June 8 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1969 November 16 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2A. LV Family: DF-3. Launch Vehicle: Chang Zheng 1. FAILURE: The program distributor in the second stage broke down. The rocket crashed into the earth within view of the launch site after 69 seconds of flight.. Failed Stage: 2.
1970 April 24 - . LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1970 April 24 - . 13:35 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2A. LV Family: DF-3. Launch Vehicle: Chang Zheng 1.
1971 March 3 - . 12:15 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2A. LV Family: DF-3. Launch Vehicle: Chang Zheng 1.

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