UniSat-6

{{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 = [http://www.gaussteam.com/unisat-6-mission/ 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 =

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}}

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.{{Cite web|url=http://space.skyrocket.de/doc_sdat/unisat-6.htm|title = UniSat 6}}

Launch

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

Mission

File:Unisat-6 integration.jpg launcher.]]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,{{cite web |url=http://www.tigrisatcubesat.com/ |title=Tigrisat CubeSat - Home |access-date=2015-09-25 |url-status=dead |archive-url=https://web.archive.org/web/20150925090543/http://www.tigrisatcubesat.com/ |archive-date=2015-09-25 }} with a total volume 9U. All sub-satellites were deployed 25 hours after achieving orbit, without incidents.{{Cite web|url=http://www.gaussteam.com/unisat-6-cubesat-release-accomplished/|title=UNISAT-6 CubeSat release accomplished – GAUSS SRL – Italy}}

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

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See also

{{Portal|Spaceflight}}

References

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