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词条 UniSat-6
释义

  1. Launch

  2. Mission

  3. See also

  4. References

  5. External links

{{Infobox spaceflight
| name = UNISAT-6
| names_list =


| image = Unisat-6 patchMission-500x500.png
| image_caption = UNISAT-6 Mission Patch
| image_alt =
| image_size = 200px
| mission_type = Technology demonstration
| operator = GAUSS Srl
| Harvard_designation =
| COSPAR_ID = 2014-033C
| SATCAT = 40012
| website = GAUSS Srl page on UniSat-6 mission
| mission_duration =
| distance_travelled =
| orbits_completed =
| suborbital_range =
| suborbital_apogee =
| spacecraft =
| spacecraft_type =
| spacecraft_bus =
| manufacturer =
| launch_mass = {{convert|26|kg|abbr=on}}
| BOL_mass =
| landing_mass =
| dry_mass =
| payload_mass =
| dimensions =
| power =
| launch_date = {{start date and age|df=yes|2014|06|19}}
| launch_rocket = Dnepr
| launch_site = Dombarovsky site 13
| launch_contractor =
| deployment_from =
| deployment_date =
| entered_service =
| disposal_type =
| deactivated =
| destroyed =
| last_contact =
| recovery_by =
| recovery_date =
| decay_date =
| landing_date =
| landing_site =


| orbit_reference = Geocentric
| orbit_regime = Sun Synchronous
| orbit_longitude =
| orbit_slot =
| orbit_semimajor =
| orbit_eccentricity = 0.005957
| orbit_periapsis = 610 km
| orbit_apoapsis = 694 km
| orbit_inclination = 97.93 °
| orbit_period =
| orbit_RAAN =
| orbit_arg_periapsis =
| orbit_mean_anomaly =
| orbit_mean_motion =
| orbit_repeat =
| orbit_velocity =
| orbit_epoch =
| orbit_rev_number =
| apsis = gee


| programme =
| previous_mission =
| next_mission =
| insignia =
| insignia_caption =
| insignia_alt =
| insignia_size =
}}UniSat-6 is an Italian micro-satellite developed by GAUSS Srl and launched in 2014. The satellite is built in a 0.4x0.4x0.4m box-shaped bus, optimized for piggy-back launch. All instruments are powered by solar cells mounted on the spacecraft body, with maximal electrical power of 11W. The satellite has no on-orbit propulsion, it makes use of an attitude stabilization system based on permanent magnets.[1]

Launch

UniSat-6 was launched from Dombarovsky (air base) site 13, Russia, on 19 June 2014 by a Dnepr rocket.

Mission

The satellite is intended primarily for technology verification in space, the main test piece being 3 deployment systems loaded with 4 CubeSat satellites, namely AeroCube 6, Lemur 1, ANTELSAT and Tigrisat,[2] with a total volume 9U. All sub-satellites were deployed 25 hours after achieving orbit, without incidents.[3]

The satellite is also equipped with an on-board camera to take pictures of the release of the cubesats and for Earth Observation.

{{clear}}

See also

{{Portal|Spaceflight}}
  • 2014 in spaceflight

References

1. ^http://space.skyrocket.de/doc_sdat/unisat-6.htm
2. ^{{cite web |url=http://www.tigrisatcubesat.com/ |title=Archived copy |accessdate=2015-09-25 |deadurl=yes |archiveurl=https://web.archive.org/web/20150925090543/http://www.tigrisatcubesat.com/ |archivedate=2015-09-25 |df= }}
3. ^http://www.gaussteam.com/unisat-6-cubesat-release-accomplished/

External links

{{Orbital launches in 2014}}{{Italy-spacecraft-stub}}

6 : Student satellites|Satellites of Italy|Spacecraft launched in 2014|2014 in Italy|CubeSats|Spacecraft launched by Dnepr rockets

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