
Aeros 2 [DLR]
The Aeros satellites had a circular cylindrical shape, 0.91 m in diameter and 0.71 m in height. It was launched into an elliptical, polar, nearly sun-synchronous earth orbit. The spacecraft was spin stabilized at 10 rpm and oriented with the spin axis toward the sun. The purpose of the mission was to study the state and behavior of the upper atmosphere and ionospheric F region, especially with regard to the influence of solar ultraviolet radiation. Five experiments provided data on the temperature and density of electrons, ions, and neutral particles, the composition of ions and neutral particles, and solar ultraviolet flux.
| Nation: | Germany |
|---|---|
| Type / Application: | Research |
| Operator: | Bundesministerium für Bildung und Wissenschaft, NASA |
| Contractors: | Dornier |
| Equipment: | |
| Configuration: | Spin stabilized |
| Propulsion: | |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | 127 kg |
| Orbit: | 223 km × 867 km, 96.9° (#1); 217 km × 879 km, 97.4° |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| Aeros 1 | 16.12.1972 | Va SLC-5 | Scout-D1 | ||
| Aeros 2 | 16.07.1974 | Va SLC-5 | Scout-D1 |