E-st@r-II

Summary

e-st@r-II
E-st@r-II before launch
Mission typeTechnology
OperatorPolitecnico di Torino
COSPAR ID2016-025D
SATCAT no.41460
Spacecraft properties
Spacecraft type1U CubeSat
Launch mass1 kilogram (2.2 lb)
Start of mission
Launch date25 April 2016 21:02 (2016-04-25UTC21:02Z)
RocketSoyuz
Launch siteKourou ELV
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeLow Earth (SSO)
Perigee altitude449.4 kilometres (279.2 mi)
Apogee altitude693.7 kilometres (431.0 mi)
Inclination98.2 degrees
Period95.9  minutes
 

e-st@r-II (Educational Satellite @ Polytechnic University of Turin 2) is a miniaturized satellite designed and built by Polytechnic University of Turin, as part of the "Fly Your Satellite" program of the European Space Agency.

Launch and deployment

It is a CubeSat satellite, placed in orbit by Arianespace with Soyuz Booster, VS14 flight, on April 25, 2016 at 21:02 GMT (23:02 CEST) from Europe's spaceport in Kourou, French Guiana . The main payload of the launch was Sentinel-1B from program Copernicus and Microscope designed by the CNES, the French space agency.

In addition to e-st@r-II there was other two CubeSats 1U (AAUSAT 4, .htm OUFTI 1[permanent dead link]) they were packed aboard the Soyuz. These small satellites, each measuring just 10 × 10 × 11 cm in height, have been developed by teams of university students through ESA programs.

E-st@r-II is the successor of e-st@r, the first Italian CubeSat and the first CubeSat of the Polytechnic University of Turin.

More than 30 students have been working on this project, with the unique opportunity of practical experience of space applications.

E-st@r-II is a 1U CubeSat developed for demonstrating the autonomous active attitude control capabilities based on magnetic actuation: in fact, the payload is an Active Attitude Determination and Control System. The commissioning phase foresees that the payload is deactivated leaving the satellite in its free tumbling motion, without any attitude stabilization. The A-ADCS starts its work when commanded from GCS, controlling the angular velocities and the attitude of the satellite.

The primary scientific objectives of e-st@r-II mission are:

  • to demonstrate the capability of autonomous determination, control and manoeuver, through the development and test in orbit of an A-ADCS entirely designed and manufactured by students
  • to test in orbit COTS technology and self-made hardware

E-st@r-II is a follow-on of e-st@r-I, the first Italian CubeSat and the first satellite of Politecnico di Torino to be inserted on orbit. More than 30 students worked on this project, using a unique opportunity of hands-on experience on space applications. It will demonstrate the ability of determining (with gyros and magnetometers) and actively controlling its attitude. The bus functionalities, as a basis for other CubeSats, will be demonstrated: it is a step towards future missions and applications.

Currently the team that developed the satellite, the CubeSatTeam of Politecnico di Torino, is actively working on the development of the Next model: 3-STAR, a 3U CubeSat.

Communications Issues

Once deployed into orbit, e-st@r-II was designed to begin transmitting signals to Earth approximately 30 minutes after activation. Signals could be picked up by anyone with common amateur radio equipment. To celebrate the launch of this second CubeSat, members of the world amateur radio community were invited in a contest to listen for the satellite. While transmissions from the satellite were received by multiple ground stations following deployment, the received signal was not strong enough for either radio amateurs or the satellite's dedicated ground station to demodulate. An analysis of the received signal strength gave figures up to 15 dB lower than what was estimated from pre-launch link budget calculations. Ground tests using prototype hardware and flight spares were able to determine that the antenna likely did deploy correctly and the probable cause of the discrepancy was attributed to improper assembly of the satellite's RF hardware, leading to a large degree of mismatch loss. Ultimately, stations employing high-gain antennas were able to demodulate e-st@r-II's transmitted data packets and the error did not constitute a mission failure.[1]

See also

References

  1. ^ Stesina, Fabrizio; Corpino, Sabrina (1 April 2020). "Investigation of a CubeSat in Orbit Anomaly through Verification on Ground". Aerospace. 7 (4): 38. doi:10.3390/aerospace7040038.

External links

  • Official Site
  • E-st@r-II Position
  • Data