ANS 1 [NASA] |
The ANS (Astronomical Netherlands Satellite) was an sun-synchronous satellite, designed
as an astronomical observatory. The spacecraft was attitude-controlled by magnetic coils
interacting with the earth's magnetic field, by reaction wheels, and by a so-called
"yo-yo" (a device for initially despinning the spacecraft by ejecting two masses
that carry away most of the angular momentum). Attitude sensing was carried out by solar
sensors (coarse, intermediate, and fine), horizon sensors, a star sensor, and a
magnetometer. Two guide stars near the object being observed served as the final pointing
references. Experiments on board observed celestial objects in UV and X-ray wavelengths.
During its observing lifetime of 20 months (September 1974 to June 1976), ANS measured the
positions, spectra, and time variations of galactic and extragalactic X-ray sources in the
energy range 2 to 15 keV, and obtained over 18000 observations of about 400 objects in the
UV range 1500 to 3300 Angstrom.
| Nation: | Netherlands |
|---|---|
| Type / Application: | Astronomy (UV, X-ray) |
| Operator: | |
| Contractors: | ICANS |
| Equipment: | |
| Configuration: | |
| Propulsion: | |
| Lifetime: | |
| Mass: | 130 kg |
| Orbit: | 266 km x 1176 km, 98° |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| ANS 1 | 30.08.1974 | Va SLC-5 | Scout-D1 |
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs