ZA-AeroSat [Stellenbosch University]
ZA-AeroSat is a 2U-CubeSat for technolgy development and upper atmosphere science. It is developed and built at the Stellenbosch University, South Africa.
The satellite carries four feather communication antennas, which are also used for passive aerodynamic stabilisation. An active momentum wheel and magnetic stabilisation control system will be used to damp the aerodynamic oscillations and reduce the attitude disturbances.
The satellite will use magnetic sensors and actuators to do initial detumbling into a Y-Thompson spin after release from its deployer. After a set time after release, all deployables, including the antennas, will deploy. The satellite will then start transmitting a beacon, and start listening for communication from a groundstation. When the appropriate command is received, the satellite will activate its full suite of sensors and actuators to orientate itself in the RAM direction. During this process the spin the satellite contains in the Y-axis, is absorbed into a momentum wheel, which then provides the stabilized satellite with a momentum bias. At this point the QB50 science payload will be activated and occasionally the payload star camera will be tested. In the case of a fault in the communications is detected throughout the mission, the secondary communications unit will be activated. Science data, telemetry data, as well as images captured by the star and Nadir cameras will be sent to the ground station with each communications opportunity.
It is a part of the QB50 constellation to gather science data in the upper layers of the troposphere in the altitude range from 350 km down to 200 km. The QB50 project, which will demonstrate the possibility of launching a network of 50 CubeSats built by Universities Teams all over the world as a primary payload on a low-cost launch vehicle to perform first-class science in the largely unexplored lower thermosphere.
The satellite will be launched with the bulk of the QB50 constellation to the ISS in 2017, from where they will be deployed. The in-orbit lifetime of ZA-AeroSat is about 3 months, from deployment to de-orbit.
|Type / Application:||Technology, atmosphere|
|Power:||Solar cells, batteries|
|Orbit:||400 km × 400 km, 51°|
|ZA-AeroSat (QB50 AZ01)||-||2017||CC SLC-41||Atlas-5(401)||with Cygnus CRS-7, ALTAIR 1, SUSat, UNSW-EC0, i-INSPIRE 2, nSIGHT 1, Ex-Alta 1, LilacSat 1, NJUST 1, Aoxiang 1, SOMP 2, QBITO, Aalto 2, X-CubeSat, SpaceCube, DUTHSat, UPSat, Hoopoe, LINK, SNUSAT 1, SNUSAT 1b, qbee50-LTU-OC, BeEagleSat, HAVELSAT, Phoenix, PolyITAN-2-SAU, QBUS 1, QBUS 2, QBUS 4, IceCube, CSUNSat 1, CXBN 2, Biarri-Point, Lemur-2 30, ..., 34?|