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Delfi-C3

Delfi-C3 is a CubeSat satellite constructed by students at the Delft University of Technology in the Netherlands. It is a 3-unit CubeSat,[1] and was launched at 03:53:42 on 28 April 2008,[2] as part of the NLS-4 mission,[3] aboard a PSLV rocket, from the Second Launch Pad at the Satish Dhawan Space Centre in India. The launch was contracted by ISRO, through Antrix Corporation and UTIAS.[3]

Delfi-C3
Delfi-C3 in stowed configuration
Mission typeTechnology
OperatorDelft University of Technology
COSPAR ID2008-021G
SATCAT no.32789
WebsiteDelfi-C3 - Home
Mission duration15 years, 6 months and 9 days (in progress)
Spacecraft properties
Bus3U CubeSat[1]
Launch mass2.2 kilograms (4.9 lb)
Power2.5 watts
Start of mission
Launch date28 April 2008 (2008-04-28)
RocketPSLV-CA C9
Launch siteSatish Dhawan SLP
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
 

The satellite's primary mission is technology demonstration and development.[4] It is carrying new types of solar cells,[4] a solar sensor for TNO Science and Industry,[4] and a high-efficiency amateur radio transceiver experiment.[4]

Delfi-C3 does not contain batteries, as the experiments are dependent on the sun. She is the fourth Dutch Satellite, after ANS, IRAS and SLOSHSAT. It is the first Dutch university Satellite and is based on a 3-Unit CubeSat.

Some other mission characteristics include:

The Delfi-C3 ground segment consists of two command ground stations, the primary being in Delft and the backup station at the TU Eindhoven in Eindhoven. For data collection, a distributed ground station network (DGSN) is used in which radio amateurs receive packets and sent these via internet to the central data collection server. Data decoding is possible with the free RASCAL software provided by the Delfi-C3 team.

The Delfi-C was still largely operational when it was followed up by the Delfi-n3Xt on October 21, 2013.

In May 2008, the amateur radio payload on the satellite was designated Delfi-C3 OSCAR-64 or Dutch OSCAR-64 (DO-64).[5]

See also edit

References edit

  1. ^ a b . Archived from the original on 2011-09-27. Retrieved 2008-05-16.
  2. ^ . Archived from the original on 2008-05-21. Retrieved 2008-05-16.
  3. ^ a b UTIAS - NLS-4
  4. ^ a b c d . Archived from the original on 2011-09-27. Retrieved 2008-05-16.
  5. ^ "AMSAT News Service Bulletin 138.02". Radio Amateur Satellite Corporation. 2008-05-18. Retrieved 2016-12-11.

delfi, cubesat, satellite, constructed, students, delft, university, technology, netherlands, unit, cubesat, launched, april, 2008, part, mission, aboard, pslv, rocket, from, second, launch, satish, dhawan, space, centre, india, launch, contracted, isro, throu. Delfi C3 is a CubeSat satellite constructed by students at the Delft University of Technology in the Netherlands It is a 3 unit CubeSat 1 and was launched at 03 53 42 on 28 April 2008 2 as part of the NLS 4 mission 3 aboard a PSLV rocket from the Second Launch Pad at the Satish Dhawan Space Centre in India The launch was contracted by ISRO through Antrix Corporation and UTIAS 3 Delfi C3Delfi C3 in stowed configurationMission typeTechnologyOperatorDelft University of TechnologyCOSPAR ID2008 021GSATCAT no 32789WebsiteDelfi C3 HomeMission duration15 years 6 months and 9 days in progress Spacecraft propertiesBus3U CubeSat 1 Launch mass2 2 kilograms 4 9 lb Power2 5 wattsStart of missionLaunch date28 April 2008 2008 04 28 RocketPSLV CA C9Launch siteSatish Dhawan SLPOrbital parametersReference systemGeocentricRegimeLow Earth The satellite s primary mission is technology demonstration and development 4 It is carrying new types of solar cells 4 a solar sensor for TNO Science and Industry 4 and a high efficiency amateur radio transceiver experiment 4 Delfi C3 does not contain batteries as the experiments are dependent on the sun She is the fourth Dutch Satellite after ANS IRAS and SLOSHSAT It is the first Dutch university Satellite and is based on a 3 Unit CubeSat Some other mission characteristics include No active attitude control 1200Bd BPSK VHF downlink Linear transponderThe Delfi C3 ground segment consists of two command ground stations the primary being in Delft and the backup station at the TU Eindhoven in Eindhoven For data collection a distributed ground station network DGSN is used in which radio amateurs receive packets and sent these via internet to the central data collection server Data decoding is possible with the free RASCAL software provided by the Delfi C3 team The Delfi C was still largely operational when it was followed up by the Delfi n3Xt on October 21 2013 In May 2008 the amateur radio payload on the satellite was designated Delfi C3 OSCAR 64 or Dutch OSCAR 64 DO 64 5 See also editList of CubeSatsReferences edit a b Delfi C3 Delfi C3 Satellite Archived from the original on 2011 09 27 Retrieved 2008 05 16 Delfi C3 Mission Status Page Archived from the original on 2008 05 21 Retrieved 2008 05 16 a b UTIAS NLS 4 a b c d Delfi C3 Mission Overview Archived from the original on 2011 09 27 Retrieved 2008 05 16 AMSAT News Service Bulletin 138 02 Radio Amateur Satellite Corporation 2008 05 18 Retrieved 2016 12 11 Retrieved from https en wikipedia org w index php title Delfi C3 amp oldid 1182500850, wikipedia, wiki, book, books, library,

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