Jump to content

Bhaskara (satellites)

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by GreenC bot (talk | contribs) at 18:15, 17 November 2016 (1 archive template merged to {{webarchive}} (WAM)). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

1984 USSR stamp featuring Bhaskara-I, Bhaskara-II and Aryabhata satellites

The Bhaskara-I and II Satellites were two satellites built by the Indian Space Research Organisation that formed India's first low orbit Earth Observation Satellite. They collected data on telemetry, oceanography and hydrology.

Bhaskara-I

Bhaskara-I
Mission typeExperimental Remote Sensing
Earth Obsservation Satellite
Mission duration10 years (Re-Entered in 1989)[1]
Spacecraft properties
Spacecraft typeUnmanned
ManufacturerIndia ISRO
Launch mass444 kilograms (979 lb)
Power47 watts
Start of mission
Launch date7 June 1979 (1979-06-07Z) IST
RocketC-1 Intercosmos Launch Vehicle
Launch siteKapustin Yar

Bhaskara-I, weighing 444 kg at launch, was launched on 7 June 1979 from Kapustin Yar aboard the Intercosmos launch vehicle. It was placed in an orbital Perigee and Apogee of 394 km and 399 km at an inclination of 50.7°.[2] The satellite consisted of-

  • Two television cameras operating in visible (600 nanometre) and near-infrared (800 nanometre) and collected data related to hydrology, forestry and geology.
  • Satellite microwave radiometer (SAMIR) operating at 19 and 22 GHz for study of ocean-state, water vapour, liquid water content in the atmosphere, etc.

Bhaskara-II

Bhaskara-II
Mission typeExperimental Remote Sensing
Earth Obsservation Satellite
Mission duration10 years (Re-Entered in 1991)
Spacecraft properties
Spacecraft typeUnmanned
ManufacturerISRO
Launch mass444 kilograms (979 lb)
Power47 watts
Start of mission
Launch date20 November 1981 (1981-11-20Z) IST
RocketC-1 Intercosmos Launch Vehicle
Launch siteVolgograd Launch Station

The satellite provided ocean and land surface data. It orbited at 541 x 557 km with inclination of 50.7°. One of two onboard cameras malfunctioned, however it sent back more than two thousand images. Housekeeping telemetry was received until re-entry in 1991.[3]

See also

References