Encyclopedia Astronautica
Shanghai


Chinese manufacturer of rocket engines and rockets. Shanghai Institute of Electro-mechanical Design, Shanghai, China.

AKA: SAST.
Location: Shanghai.

More... - Chronology...


Associated Countries
Associated Engines
See also
Associated Launch Vehicles
  • T-7M Chinese sounding rocket. 2 stage test vehicle for T-7. More...
  • T-7 Chinese sounding rocket. China's first sounding rocket and first indigenously-built sounding rocket, launched from 1960-1965. The basic vehicle consisted of a single liquid propellant stage. This was later augmented with solid propellant booster stages. Later versions dispensed with the liquid propellant stage. More...
  • T-7A Chinese sounding rocket. Boosted version of China's first indigenously-built sounding rocket. Included solid propellant booster. The upper stage and payload were recovered by parachute and reused. Launches began in 1965. Consisted of a solid propellant booster mated to the basic liquid propellant T-7. Flown from 1965 to the end of the 1960's. More...
  • T-7/GF-01A Chinese sounding rocket. Three stage vehicle consisting of T-7A + GF-01A More...
  • HP2 Chinese sounding rocket. Two-stage solid propellant sounding rocket. Evidently used two of the first stage motors developed for the T-7A in tandem. Replaced the T-7 from 1970 on. Used for routine measurement of the upper atmosphere. More...
  • HP6 Chinese sounding rocket. Lightweight single stage solid propellant sounding rocket. Used for routine measurement of the upper atmosphere. More...
  • 761 Chinese sounding rocket. Lightweight two-stage solid propellant sounding rocket. Designation indicates development was authorised in January 1976. Evidently replaced both the HP2 and HP6 from about 1980 on. Used for routine measurement of the upper atmosphere. More...
  • Project 921 In 1992 Xiandong Bao of the Shanghai Astronautics Bureau revealed plans for a modular family of modern rockets to support future Chinese manned space activities. The entire family would be based on a Lox/Kerosene booster stage of 306 tonnes mass, and a Lox/LH2 upper stage of 57 tonnes mass. More...

Associated Stages

Shanghai Chronology


1960 February 19 - . Launch Site: Laogang. LV Family: T-7. Launch Vehicle: T-7M.
  • Test mission - . Nation: China. Agency: Shanghai. Apogee: 8.00 km (4.90 mi). The Shanghai design institute completed the first subscale experimental model of the T-7 sounding rocket. This would use a solid booster and liquid propellant sustainer stage. The rocket was fuelled using a bicycle pump. Launched from Laogang, on the coast, the missile reached 8 km altitude.

1960 September 1 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7.
  • Test mission - . Nation: China. Agency: Shanghai. Apogee: 60 km (37 mi). Summary: First launch of the all-up missile..

1963 December 1 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7A.
  • Test mission - . Nation: China. Agency: Shanghai. Apogee: 115 km (71 mi).

1964 July 19 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7A-S.
  • Life Science (mice) Biological mission - . Nation: China. Agency: Shanghai. Apogee: 70 km (43 mi).

1965 June 1 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7A-S.
  • Life Science (mice) Biological mission - . Nation: China. Agency: Shanghai. Apogee: 70 km (43 mi).

1965 June 5 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7A-S.
  • Life Science (mice) Biological mission - . Nation: China. Agency: Shanghai. Apogee: 70 km (43 mi).

1966 July 14 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7A-S2.
  • Life Science (dog) Biological mission - . Nation: China. Agency: Shanghai. Apogee: 100 km (60 mi).

1966 July 28 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7A-S2.
  • Life Science (dog) Biological mission - . Nation: China. Agency: Shanghai. Apogee: 100 km (60 mi).

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