TD 1A / 1972 - 014A
Spacecraft propulsion supplied by ArianeGroup
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TD 1A / 1972 - 014A
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Category | Science |
| Operator | ESRO (ESA) | |
| Orbit | LEO | |
| Sat position | 524 km x 551 km | |
| Launch date | 12.3.1972 | |
| Launch mass | 472 kg | |
| Design life | 2 years | |
| Launcher | Thor-Delta-N | |
| Satellite / Bus | Intelsat 3 Bus | |
| Manufacturer | Hawker Siddeley Dynamics | |
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Orbital Propulsion Centre Contribution
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Argon Gas
Tank, 280 bar