AAUsat-2

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Organization
AAU StudentSpace
Launch Date
28th April 2008
Launch Site
Satish Dhawan Space Centre
Launcher
PSLV
Dimensions
10 x 10 x 11,3 cm³
Satellite Mass
1 Kg

AAUSAT-II is the second student-built CubeSat built and operated by students from University of Aalborg in Denmark. It was launched 28 April 2008 05:54 UTC from Satish Dhawan Space Centre in India on a PSLV rocket. AAUSAT-II carries a radiation sensor.

Contents

[edit] The educational objective

The primary purpose of construction of satellites at Aalborg University is to give the students engineering capabilities beyond what is normally achieved within a master study.

[edit] History

Student satellite activities at Aalborg University (AAU) started in 2003 as a result of AAU's involvement in the first pure Danish research satellite, Ørsted, which was successfully launched in 1999.

AAUSAT-II's predecessor was AAU CubeSat which was constructed in the period 2001-2003 and was launched 30 June 2003.

The construction of AAUSAT-II began in 2005.

[edit] Operations

After launch April 28th 2008 AAUSAT-II beacon was received at CalPoly University in California.

The following weeks beacons was received but no two way communication was obtained.

It turned out that AAUSAT-II was transmitting at a lower level than anticipated.

Afterwards the ground station has been upgraded, resulting in fully functional two way communication.

[edit] Mission definition

AAUSAT-II consists of several sub-systems:

  • ADCS: Attitude Determination and Control System
  • CDH: Command and Datahandling System
  • COM: Communication System
  • EPS: Electrical Power System
  • GND: Ground Station
  • MCC: Mission Control Center
  • MECH: Mechanical System
  • OBC: On-board Computer System
  • P/L: Payload System


Technical Facts:

Dimensions 100 × 100 × 113 mm Cubesat standard
Mass 750 gram
Expected lifetime Minimum 1 month, extended until end of lifetime
Attitude determination system Sun sensors, gyro sensors, magnetometers
Attitude control system Momentum wheel and magnetic coils
Power Solar-cell panels located in satellite surface
Batteries Li-ion 8.2V 2200 mAh
Power bus 3.3 and 5V regulated

[edit] HAM information

  • Callsign: OZ2CUB
  • Up/downlink: 437.425 MHz AFSK & FSK
  • Bit rate: 1200-9600 bit/s (1200 as standard mode)
  • AX.25 FM CW TLM

[edit] External links

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