AAU CubeSat
Computer simulated image of AAU CubeSat in orbit around Earth
NamesAalborg University CubeSat
AAUSat-1
Mission typeTechnology demonstration
OperatorAAU Student Space
COSPAR ID2003-031G Edit this at Wikidata
SATCAT no.27846
Websitewww.aausatii.aau.dk
Mission duration1 month (planned)
2.5 months (achieved)
Spacecraft properties
SpacecraftAalborg University CubeSat
Spacecraft type1U CubeSat
BusCubeSat
ManufacturerAAU Student Space
Launch mass1 kg (2.2 lb)
Dimensions10 × 10 × 10 cm (3.9 × 3.9 × 3.9 in)
Start of mission
Launch date30 June 2003, 14:15:26 UTC[1]
RocketRokot No. 7
Launch sitePlesetsk, Site 133/3
ContractorKhrunichev State Research and Production Space Center
Orbital parameters
Reference systemGeocentric orbit[2]
RegimeSun-synchronous orbit
Perigee altitude818 km (508 mi)
Apogee altitude830 km (520 mi)
Inclination98.7°
Period101.4 minutes
 

AAU CubeSat was a CubeSat built and operated by students from Aalborg University in Denmark. AAU CubeSat was launched on 30 June 2003 from the Plesetsk Cosmodrome on a Russian Rockot launch vehicle.[3]

The satellite was alive for two and a half months, during which some data was received on Earth; however, it was never possible to establish a solid communication link. It is thought that there was a problem with the on-board transmitter.

Spacecraft

The aluminium frame was milled from a solid block to ensure that a strong and lightweight frame was created. There are four rails to allow the satellite to slide in and out of the frame. The four rails are connected by other aluminium pieces. The subsystem circuit boards are screwed onto these pieces. Carbon-fiber plates are then glued onto the outside of the frame to support the solar panels and attitude control coils. The solar panels and attitude control coils are glued to the plates.[4]

Payload

AAU CubeSat's payload is a CMOS digital camera. It has a resolution of 1.3 megapixels and has a color depth of 24 bit. From the satellite's 830-kilometre (520 mi) altitude, the camera will capture pictures with a resolution of 120 by 110 metres (390 ft × 360 ft) per pixel. The camera-chip was provided by a company called Devitech which is in Aalborg. The Copenhagen Optical Group and the mechanical group developed the lens system. The structure for the lens system is made out of titanium.[4]

Communications

The communications systems on the satellite are composed of a modem and a radio. The radio is a SX450 type radio from Wood and Douglas. It broadcasts at 500 mW. The modem is a MX909 chip. It runs at 9600 baud and has many features such as:

Attitude Determination and Control System

The ADCS aims the camera in the right direction, (away from the Sun) and positions all three sides with solar panels to be facing the Sun for maximum power output. The satellite is positioned by three coils of wire that generate a magnetic field that interacts with Earth's magnetic field. These interactions change the attitude and orientation of the satellite. The sensor array that determines attitude is made up of a magnetometer and a Sun sensor. The magnetometer was provided by Honeywell and determines the direction of Earth's magnetic field. The Sun sensors are planar photo diodes that detect the intensity of incoming sunlight.[4]

Specifications

See also

References

  1. ^ McDowell, Jonathan (21 July 2021). "Launch Log". Jonathan's Space Report. Retrieved 28 October 2021.
  2. ^ "AAU CubeSat". NASA. 21 October 2021. Retrieved 28 October 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  3. ^ Lars Alminde; Morten Bisgaard; Dennis Vinther; Tor Viscor; Kasper Ostergard (2003), "Educational Value and Lessons Learned from the AAU-Cubesat Project", Recent Advances in Space Technologies, Institute of Electrical and Electronics Engineers (3): 57, Bibcode:2003rast.conf...57A, ISBN 0-7803-8142-4, retrieved 28 October 2021
  4. ^ a b c d "AAU CubeSat Homepage".
  5. ^ "AAU CubeSat". Gunter's Space Page. 6 August 2020. Retrieved 28 October 2021.

External links

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