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Quakesat

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Quakesat
Mission typeEarth observation
COSPAR ID2003-031FEdit this at Wikidata
SATCATno.27845
Website[1]
Mission duration21 years and 16 days (elapsed)
Spacecraft properties
SpacecraftCubeSat
Spacecraft type3CubeSat
ManufacturerStanford University
Launch mass5 kg (11 lb)
Start of mission
Launch date30 June 2003, 14:15:26UTC
RocketRockot/Briz-KM
Launch sitePlesetsk Cosmodrome,Site 133
ContractorKhrunichev State Research and Production Space Center
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeLow Earth orbit
Perigee altitude821 km (510 mi)
Apogee altitude833 km (518 mi)
Inclination98.70°
Period101.40 minutes
Instruments
Magnetometer

Quakesatis anEarth observationnanosatellitebased on threeCubeSats.It was designed to be a proof of concept for space-based detection ofextremely low frequencysignals, thought by some to beearthquakeprecursor signals. The science behind the concept is disputed.[2]

Mission[edit]

The students working on the project hope that the detection of magnetic signals may have value in showing the onset of an earthquake.[3]QuakeFinder,the company that put the satellites together, is fromPalo Alto, California.They are gathering data on the extremely lowmagnetic fieldfluctuations that are associated with earthquakes to help better understand this area of study. The primary instrument is amagnetometerhoused in a 2 ft (0.6 m) telescoping boom.

The 30 June 2003, deployment of Quakesat was alongside other university CubeSats and one commercial CubeSat. The launch occurred on aRokotrocket from Russia'sPlesetsk Cosmodrome.

See also[edit]

References[edit]

  1. ^"Trajectory: Quakesat 2003-031F".NASA. 14 May 2020.Retrieved16 December2020.Public DomainThis article incorporates text from this source, which is in thepublic domain.
  2. ^
  3. ^Malik, Tariq (2003)."What's Shakin'? Tiny Satellite to Try and Predict Earthquakes".Space. Archived fromthe originalon 24 July 2008.Retrieved8 December2008.

QuakeFinder LLC Single axis search coil, small E-field dipole[2]