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Class: Earth. Type: Atmosphere. Destination: Maximum Payload Orbit. Nation: Italy. Agency: CRS. Atmospheric density studies. Typical orbit: 235 x 758 km, 9.9 deg inclinaton.
San Marco Chronology - 1964 December 15 - San Marco 1 - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Vehicle: Scout. Mass: 254 kg (559 lb). Perigee: 200 km (120 mi). Apogee: 842 km (523 mi). Inclination: 37.80 deg. Period: 95.10 min.
Atmospheric density studies. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).
- 1967 April 26 - San Marco 2 - Launch Site: San Marco. Launch Complex: -. Launch Vehicle: Scout. Mass: 129 kg (284 lb). Perigee: 219 km (136 mi). Apogee: 741 km (460 mi). Inclination: 2.90 deg. Period: 94.20 min.
Atmospheric density data. Scientific satellite launched from a mobile range off Formosa Bay (Kenya).
- 1971 April 24 - San Marco 3 - Launch Site: San Marco. Launch Complex: -. Launch Vehicle: Scout. Mass: 164 kg (361 lb). Perigee: 222 km (137 mi). Apogee: 707 km (439 mi). Inclination: 3.20 deg. Period: 93.80 min.
Atmospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).
- 1974 February 18 - San Marco 4 - Launch Site: San Marco. Launch Complex: -. Launch Vehicle: Scout. Mass: 164 kg (361 lb). Perigee: 270 km (160 mi). Apogee: 875 km (543 mi). Inclination: 2.90 deg. Period: 96.10 min.
Measurement of density, temperature, composition of atmosphere. Launch time 10:05:28.5 GMT. Anticipated life: 3 years.
- 1988 March 25 - San Marco D/L - Launch Site: San Marco. Launch Complex: -. Launch Vehicle: Scout. Mass: 236 kg (520 lb). Perigee: 268 km (166 mi). Apogee: 625 km (388 mi). Inclination: 3.00 deg. Period: 93.50 min.
Upper atmosphere studies; US, France, Italy participation.
Bibliography:
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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