Astrid_(satellite) Knowpia

Astrid 1 and Astrid 2
Operator	Swedish National Space Board
COSPAR ID	Astrid 1: 1995-002B; Astrid 2: 1998-072B
SATCAT no.	Astrid 1: 23464; Astrid 2: 25568
Website	Astrid-1 at SSC Astrid-2 at SSC
Mission duration	Astrid 1: 246 days; Astrid 2: 226 days
Spacecraft properties
Manufacturer	Swedish Space Corporation
Launch mass	Astrid 1: 27 kg (60 lb); Astrid 2: <30 kg (66 lb)
Power	Astrid 1: 11.88 W (payload), 38.5 W (nominal); Astrid 2: 16 W (payload), 90 W (nominal)
Start of mission
Launch date	Astrid 1: 03:54:22, January 24, 1995 (UTC); Astrid 2: 11:57:07, December 10, 1998 (UTC)
Rocket	Cosmos-3M
End of mission
Disposal	Decommissioned
Deactivated	Astrid 1: September 27, 1995 (however, on March 1 the scientific instruments became inoperable); Astrid 2: July 24, 1999
Orbital parameters
Reference system	Geocentric
Perigee altitude	Astrid 1: 968 km (601 mi); Astrid 2: 968 km (601 mi)
Apogee altitude	Astrid 1: 1,026 km (638 mi); Astrid 2: 1,014 km (630 mi)
Inclination	Astrid 1: 82.9°; Astrid 2: 82.9°
Period	Astrid 1: 105 min; Astrid 2: 105 min

Astrid-1 and Astrid-2 were two microsatellites designed and developed by Swedish Space Corporation on behalf of the Swedish National Space Board. They were piggyback launched on a Cosmos-3M launch vehicle from Plesetsk, Russia. Astrid 1 on January 24, 1995, and Astrid 2 on December 10, 1998.

Astrid-1 edit

Sweden's first microsatellite was piggybacked with the launch of Tsikada, a Russian navigation satellite and FAISAT, a United States communications satellite.

It carried an Energetic Neutral Atom imager called PIPPI (Prelude in Planetary Particle Imaging), an Electron Spectrometer called EMIL (Electron Measurements - In-situ and Lightweight) and two UV imagers called MIO (Miniature Imaging Optics), one for imaging the Earth's aurora and one for observing Lyman alpha-emission from the Earth's geocorona. This payload, named after characters in Astrid Lindgren's books (the idea came from a Russian scientist ^[1]), was developed by the Swedish Institute of Space Physics in Kiruna.

On March 1, a DC to DC converter for the scientific instruments failed, possibly due to a short circuit, ending its scientific mission. However, the satellite was operated until September 27, serving as a testbed for various software algorithms and store-and-forward communications.

The entire satellite was built in a year and the cost, including launch, was 1.4 million U.S. dollars.

Astrid-2 edit

Astrid-2 was Sweden's second microsatellite and it was piggybacked with Nadezhda 5, a Russian navigation satellite on December 10, 1998, on a Kosmos-3M rocket from Plesetsk in Russia.^[2]^[3]

Its payload, built by the Swedish Institute of Space Physics in Kiruna and Uppsala and the Royal Institute of Technology (Alfven Laboratory) in Stockholm, was EMMA (Electrical and Magnetic field Monitoring of the Aurora), LINDA (Langmuir INterferometer and Density experiment for Astrid-2), MEDUSA (Miniaturized Electrostatic DUal-tophat Spherical Analyzer) and PIA (Photometers for Imaging the Aurora). It was used to explore the electric and magnetic fields in the upper ionosphere and to measure neutral and charged particles and electron density.

On July 24, 1999, the contact with the satellite was lost. During its 7+1⁄2 months in space, Astrid-2 delivered a large amount of information to researchers.

References edit

^ "Satelliter finansierade av Rymdstyrelsen" (in Swedish). Swedish National Space Board. Archived from the original on 2014-07-14. Retrieved 2014-07-07.
^ NASA Mission and Spacecraft Library Astrid-2
^ "Astrid-2". www.astronautix.com. Archived from the original on 3 March 2022. Retrieved 24 April 2022.