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Isis
 Isis 1 Credit: Manufacturer Image |
Status: Operational 1969. First Launch: 1969-01-30. Last Launch: 1971-04-01. Number: 2 . Gross mass: 253 kg (557 lb).
More at: Isis.
Family: Earth, Magnetosphere sat. Country: Canada. Launch Vehicles: Thor, Delta, Thor Delta E, Thor Delta E1. Launch Sites: Vandenberg, Vandenberg SLC2E. Agency: CRCSS. Bibliography: 2, 279, 3816, 6, 6602, 12690.
1969 January 30 - . 06:46 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Thor. Launch Vehicle: Thor Delta E1.
- Isis 1 - . Payload: Isis A. Mass: 241 kg (531 lb). Nation: Canada. Agency: CRCSS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Isis. USAF Sat Cat: 3669 . COSPAR: 1969-009A. Apogee: 3,458 km (2,148 mi). Perigee: 578 km (359 mi). Inclination: 88.40 deg. Period: 127.60 min. Ionospheric measurements; data correlated with measurements from Alouette 1. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .
1971 April 1 - . 02:57 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Thor. Launch Vehicle: Thor Delta E1.
- Isis 2 - . Payload: Isis B. Mass: 264 kg (582 lb). Nation: Canada. Agency: CRCSS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Isis. USAF Sat Cat: 5104 . COSPAR: 1971-024A. Apogee: 1,424 km (884 mi). Perigee: 1,358 km (843 mi). Inclination: 88.20 deg. Period: 113.60 min. Ionospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .
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