Explorer 32 (AE B) [NASA] |
AE B (Aeronomy Explorer B) was an aeronomy satellite
which was designed to directly measure temperatures, composition, densities, and pressures
in the upper atmosphere on a global basis. The satellite was a stainless steel,
vacuum-sealed sphere, 0.889 m in diameter. The experimental payload included one ion and
two neutral mass spectrometers, three magnetron density gauges, and two electrostatic
probes. Additional equipment included optical and magnetic aspect sensors, magnetic
attitude and spin rate control systems, and a tape recorder for data acquisition at
locations remote from ground receiving stations. Power was supplied by silver-zinc
batteries and a solar cell array mounted on the satellite exterior. Two identical
pulse-modulated telemetry systems and a canted turnstile antenna were employed. The two
neutral-particle mass spectrometers failed about 6 days after launch. The remaining
experiments operated satisfactorily and provided useful data for most of the 10-month
satellite lifetime. The spacecraft ceased to function due to battery failures which
resulted from depressurization of the sphere.
| Nation: | USA |
|---|---|
| Type / Application: | Atmospheric Research |
| Operator: | NASA |
| Contractors: | |
| Equipment: | |
| Configuration: | |
| Propulsion: | ? |
| Lifetime: | |
| Mass: | 225 kg |
| Orbit: | 282 km x 2723 km, 64.6° |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| Explorer 32 (AE B, S 6a) | 25.05.1966 | CC LC-17B | Delta-C1 |
| Further AE missions: |
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs