Pollux (D-5A) [CNES]
The French Pollux (D5-A) satellite was launched as a piggyback of the Castor (D 5B). The external structure of the D5-A was an octahedron made up of two truncated tetrahedrons, eight facets of which were covered with solar cells. The D5-A carried a hydrazine propulsion system that was tested in space.
Nation: | France |
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Type / Application: | Science |
Operator: | CNES |
Contractors: | |
Equipment: | |
Configuration: | hydrazine propulsion system |
Propulsion: | |
Power: | Solar cells, batteries |
Lifetime: | |
Mass: | 38 kg |
Orbit: | 299 km × 1258 km, 30° |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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Pollux (D 5A) | 1973-F02 | 21.05.1973 | Ko ELD | F | Diamant-B | with Castor (D 5B) |
Pollux (D 5A) | 1975-039A | 17.05.1975 | Ko ELD | Diamant-BP4 | with Castor (D 5B) |