
Minisat 01 [INTA]
Minisat, the Spanish space agency, Instituto Nacional de Tecnica Aerospacial (INTA) {195 209}kg minisatellite was launched on a Pegasus-XL from the Canary Islands (Spain) on the 21st April 1997, into a 570 km × 577 km orbit inclined at 151 degrees. The launch is reported to have cost US$10.4m. The satellite measures 1145 × 1005 × 1170 mm, with four 45 W, 1.5m deployable panels. The spacecraft power system is 28 V unregulated with 60 W average power requirement. Uplink and downlink is via S-band, 5 W at 1 Mbps, and data storage is 32Mbyte. It is 1-axis spin stabilized with an accuracy of 3 degrees. The spacecraft bus and payload roughly share 50% each of the available mass.
The satellite is built by the spanish CASA company, and the selected payload to the MINISAT 01 is composed of three instruments:
It is the first in a series of planned satellites based on this bus, and is designed to operate for 2 years.
| Nation: | Spain |
|---|---|
| Type / Application: | Experimental |
| Operator: | INTA |
| Contractors: | CASA |
| Equipment: | EURD, LEGRI, CPLM |
| Configuration: | Minisat-0 Bus |
| Propulsion: | None |
| Power: | |
| Lifetime: | |
| Mass: | 200 kg |
| Orbit: | 570 km × 577 km, 151° |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| Minisat 01 | 21.04.1997 | Ga, L-1011 | Pegasus-XL | with Celestis 01 |