e-st@r

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e-st@r
The Polytechnic University of Turin CubeSat
Namesest@r
e-star
Mission typeTechnology demonstration
OperatorPolitecnico di Torino
COSPAR ID2012-006C
SATCAT no.38079
Mission durationFinal: 4 years
Spacecraft properties
Spacecraft typeCubeSat
ManufacturerPolitecnico di Torino
Launch mass1 kg (2.2 lb)
Start of mission
Launch date13 February 2012, 10:00:00 UTC[1]
RocketVega (VV01)
Launch siteKourou, ELV
ContractorArianespace
End of mission
DisposalRe-Entry
Deactivated13 February 2016
Last contact10 February 2016
Decay date14 February 2016
Orbital parameters
Reference systemGeocentric orbit[2]
RegimeLow Earth orbit
Perigee altitude302 km (188 mi)
Apogee altitude1,082 km (672 mi)
Inclination69.47°
Period98.47 minutes

e-st@r (Educational Satellite @ Politecnico di Torino) was a miniaturised satellite built by the Politecnico di Torino.[3] It was a 1U CubeSat design with a 10 cm side and a mass not exceeding 1.33 kg.

Launch and deployment

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In 2006 the Polytechnic University of Turin had tried to put one of its satellites into orbit (PiCPoT), but the Dnepr launcher used exploded a few seconds after the start and destroyed itself.

In 2009 the European Space Agency in view of the inaugural launch of Vega (which being the first launch had a high probability of failure) offered 9 seats on the carrier for the same number of cubesats, plus another two seats for larger satellites. Only 7 of the cubesats managed to be prepared in time for launch:

They were launched into low Earth Orbit on the maiden flight of Arianespace's Vega rocket on 13 February 2012 on a multi-payload mission shared with LARES of the Italian Space Agency and ALMASat-1 of the University of Bologna.

The satellite was successfully deployed into orbit, and the signal was received by the team's ground station and by amateur radio operators.[4] However, operations have been impeded by unexpected tumbling, and the satellite was put into safe mode.[5]

The communication system used a PIC microcontroller and communicated with the ground at a frequency of 437.445 MHz with a power of 0.5 W. The frequencies had been assigned to cubesats by ESA.

A total of about 50,000 euros were spent on the design and construction of the satellite.

The orbit was inclined 71° and slightly elliptical. It also crossed the van Allen belts.

The satellite was created by the CubeSatTeam of the Polytechnic of Turin, responsible for creating picosatellites. The team later developed e-st@r-II to be sent to the orbit again as part of ESA's "Fly Your Satellite" program in 2016.[6]

See also

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References

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  1. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  2. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  3. ^ Sabrina Corpino, Nicole Viola, Fabrizio Stesina, and Sergio Chiesa, "Design and development of the e-st@r CubeSat", Paper IAC-09.B4.6B.3, 2009 International Astronautical Congress (accessed 16 August 2013)
  4. ^ E-ST@R successfully launched (accessed 16 August 2013)
  5. ^ eoPortal Directory, E-ST@R (Educational SaTellite @ politecnico di toRino) (accessed 16 August 2013)
  6. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
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