Encyclopedia Astronautica

Argentinan manufacturer of spacecraft. Instituto Universitario Aeronautico de Cordoba, Cordoba, Argentina.

Location: Cordoba.

More... - Chronology...

Associated Countries
  • Argentina The Argentine Interplanetary Society was organized in the 1940's. In 1952 Argentina was one of the founding members of the International Astronautical Federation. From 1960 the Comision Nacional de Investigaciones Espaciales (CNIE) worked with the Argentine Air Force's Instituto de Investigaciones Aeronauticas y Espaciales (IIAE) to develop indigenous sounding rockets and missiles. Argentina was the first country in Latin America to send an object into space using an indigenously-developed rocket. In the 1980's Argentina took part in a multinational effort to develop the Condor intermediate range missile. Under American pressure, the Condor Program was canceled in 1991, the IIAE and CNIE were dismantled, and further work on launch vehicles was banned. A new civilian space agency, CONAE was created, which concentrated on development of surveillance satellites for earth resource and environmental monitoring. More...

Associated Spacecraft
  • MuSat Argentinan earth magnetosphere satellite. One launch, 1996.08.29, Microsat. MuSat-1 Victor was the first Argentine-built satellite. More...

See also

Cordoba Chronology

1996 August 29 - . 05:22 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Microsat - . Payload: Victor. Mass: 32 kg (70 lb). Nation: Argentina. Agency: Cordoba. Class: Earth. Type: Magnetosphere satellite. Spacecraft: MuSat. Decay Date: 1999-11-12 . USAF Sat Cat: 24291 . COSPAR: 1996-050A. Apogee: 19,176 km (11,915 mi). Perigee: 804 km (499 mi). Inclination: 62.8000 deg. Period: 94.70 min. MuSat-1 Victor separated from the launch vehicle at 05:31 GMT, becoming the first Argentine-built satellite. Measuring 340 x 340 x 450mm."Victor " was an experimental vehicle, intended to evaluate in-orbit behaviour of low-cost space technologies. It carried two video cameras, oriented for earth-imaging, as well as transceivers in both UHF and S bands. The beacon could be heard every 90 seconds at 137.95 MHz as a brief burst of CW ("Hi hi de MUSAT"). Electrical power was provided by four 88-Si cells solar panels, with an end-of-life electrical power of 8 W. Its position was determined by means of a 3-axis, flux-gate magnetometer, as well as both solar and horizon sensors, while its attitude was 3-axis controlled by magnetic coils and reaction wheels, with a pointing precision of 0.5 deg. MuSat-1 was developed and built by a 25-person team at the Instituto Universitario Aeronautico, under the sponsorship of the government of the province of Cordoba, in a 3.5 year, $1.2 million effort.

Home - Browse - Contact
© / Conditions for Use