M-100
M-100
Credit - NASA
Sounding rocket. Year: 1957. Family: Other Suborbital Vehicles. Country: Russia.

Two-stage, solid propellant, fin stabilized, unguided Russian sounding rocket, fired in greater numbers than any other. At least 6,640 were fired to the edge of space before the vehicle was discontinued in 1990.

The M-100 is said to have begun testing in 1953, using propellant with a specific impulse of only 150 seconds. The rocket was used to make basic weather soundings on a world-wide basis. A typical flight consists of launch to 90 km altitude, following by the descent of the nosecone under a parachute over a period of 50 minutes. During the descent the payload radioed temperature, pressure, and density data. Below 50 km radar could be used to track the nose cone and determine winds aloft. In the 1970's the M-100B was cross calibrated by firing it simultaneously with American Super Loki-Dart, British Skua, and French Super-Arcas rockets. This allowed it to be integrated into the World Meteorological Rocket Network.

While the M-100 has been equipped with non-standard payloads, it was used in such numbers over such a long period that the data from the series was used to determine long-term climate trends (a steady drop in temperature of 0.3 to 1.0 deg C per year at an altitude of 80 km).

When the Soviet Union collapse, funding for state scientific work evaporated. Launches of the M-100 abruptly ended.


Number of M-100 Rockets Fired
By Year and Launch Site

YearAkitaKapustin YarKerguelenKheysaKoroniMolo dezhnayaShipShip MussonShip NoyekovShip ShirshovShip ShokalskiShip UshakovShip VoiekovThumba
1957 10 3          
1958 22 36          
1959 15 18          
1966 1            
1968 1    10       
1969 20 13 1918       
1970 42 69 44137      4
1971 57 70 4549      55
1972 45 421838   43   61
1973 4318583153  3371   64
1974 7019742250   1432  23
1975 682068354   3717  38
1976 1192075 63   5485  67
1977 8119675065   1222  59
1978 7820673164   511  60
1979 9920886163 1 1265  75
1980 8219793467   463  77
1981 9620822975   27   58
1982 83 722660   20  954
1983 41 351945   29  840
1985 41 26 32   20   30
1986 64 58 44   22  845
1987 81 962559   45  1159
1988 95 95163   16   50
1989 58 7696749  39 1 43
19902634 32 2752  19   24

Manufacturer: GMS. Launches: 6640. Launch data is: complete. Payload: 15 kg (33 lb). Apogee: 90 km (55 mi). Total Mass: 475 kg (1,047 lb). Core Diameter: 0.25 m (0.82 ft). Total Length: 8.34 m (27.36 ft). Span: 0.66 m (2.18 ft).


Model: M-100. Family: Other Suborbital Vehicles. Country: Russia.

Basic model, 4,908 fired from 1957-07-11 to 1983-09-28.


Model: M-100A. Family: Other Suborbital Vehicles. Country: Russia.

Special modification, only fired twice on 1976-11-10 and 1976-12-22.


Model: M-100B. Family: Other Suborbital Vehicles. Country: Russia.

Model calibrated with Western sounding rockets and part of the World Meteorological Network. 1,730 launched from 1976-01-07 to 1990-12-.



Bibliography and Further Reading
  • McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
  • Alway, Peter, Rockets of the World, Saturn Press, Ann Arbor, 1995. ISBN: 0962787655. Comprehensive account of world rocketry, from the beginning 'til now, from sounding rockets to Saturns. Oriented toward rocket modellers, with accurate drawings and color guides. More at amazon.com...
 
 
 
 
 
 
 
 
 

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