SNAP-1

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SNAP-1 is a British nanosatellite in low Earth orbit.[2][3] The satellite was built at the Surrey Space Centre by Surrey Satellite Technology Ltd (SSTL) and members of the University of Surrey. It was launched on 28 June 2000 on board a Kosmos-3M rocket from the Plesetsk Cosmodrome in northern Russia.[4] It shared the launch with a Russian Nadezhda search and relay spacecraft and the Chinese Tsinghua-1 microsatellite.

Mission typeTechnology
COSPAR ID2000-033C[1]
Quick facts Mission type, Operator ...
SNAP-1
Mission typeTechnology
OperatorSSTL / University of Surrey
COSPAR ID2000-033C[1]
SATCAT no.26386Edit this on Wikidata
Spacecraft properties
ManufacturerSSTL / University of Surrey
Launch mass6.5 kilograms (14 lb)
Start of mission
Launch date28 June 2000, 12:13:00 (2000-06-28UTC12:13Z) UTC
RocketKosmos-3M
Launch sitePlesetsk 132/1
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude666 kilometres (414 mi)
Apogee altitude682 kilometres (424 mi)
Inclination98.1 deg
Period98.2 minutes
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Mission

The objectives of the SNAP-1 mission were to:[2]

  • Develop and prove a modular commercial off-the-shelf (COTS) based nanosatellite bus.
  • Evaluate new manufacturing techniques and technologies.
  • Image the Tsinghua-1 microsatellite during its deployment (timed to occur a few seconds after the deployment of SNAP-1).
  • Demonstrate the systems required for future nanosatellite constellations. For example: three-axis attitude control, Global Positioning System (GPS) based orbit determination, and orbital manoeuvres.
  • Depending on propellant availability, rendezvous with Tsinghua-1 and demonstrate formation flying.

During deployment, SNAP-1 successfully imaged the Nadezhda and Tsinghua-1 satellites that accompanied it on the launch.[5][6][7] Once in orbit, SNAP-1 achieved three axis attitude control,[8] then demonstrated its orbital maintenance capability using its butane cold gas propulsion system.[9]

Architecture

The 6.5 kilograms (14 lb) SNAP-1 satellite contained the following modules:[10]

  • Power System[11]
  • VHF Receiver
  • S-band Transmitter[12]
  • Attitude and Orbit Control System (AOCS)[8]
  • Cold-Gas Propulsion (CGP) System[9]
  • On-Board Computer (OBC)
  • VHF spread-spectrum communications payload
  • UHF inter-satellite link
  • Machine Vision System (MVS)[5][6]

References

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