Aeros 1, 2

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