PSLV-C28: Difference between revisions

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{{redirect|DMC 3|the 2005 video game|Devil May Cry 3: Dante's Awakening}}
{{Infobox spaceflight
{{Infobox spaceflight
| name                 = PSLV-C28
| name               = PSLV-C28
<!--image of the spacecraft/mission-->
<!--image of the spacecraft/mission-->| image             = PSLV.svg
| image                 = PSLV.svg
| image_caption     = Model of the [[PSLV]] rocket
| image_caption         = Model of the [[PSLV]] rocket
| image_alt         = <!--image alt text-->
| image_alt             = <!--image alt text-->
| image_size         = 80px
| image_size           = 80px
<!--Basic details-->| mission_type       = Deployment of 5 [[satellite]]s.
<!--Basic details-->
| operator           = [[ISRO]] & [[Antrix Corporation]]
| mission_type         = Deployment of 5 [[satellite]]s.
| Harvard_designation = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)-->
| operator             = [[ISRO]] & [[Antrix Corporation]]
| COSPAR_ID         = 2015-032C & 2015-032D
| Harvard_designation   = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)-->
| SATCAT             = 40717 & 40718
| COSPAR_ID             = 2015-032C & 2015-032D
| website           = [http://www.isro.gov.in/ ISRO website]
| SATCAT               = 40717 & 40718
| mission_duration   = 19 minutes & 21 seconds
| website               = [http://www.isro.gov.in/ ISRO website]
| distance_travelled = 647 km
| mission_duration     = 19 minutes & 21 seconds
| orbits_completed   = <!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit-->
| distance_travelled   = 647 km
| suborbital_range   = <!--downrange distance reached if spacecraft did not enter orbit-->
| orbits_completed     = <!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit-->
| suborbital_apogee = <!--altitude reached if spacecraft did not enter orbit-->
| suborbital_range     = <!--downrange distance reached if spacecraft did not enter orbit-->
| suborbital_apogee     = <!--altitude reached if spacecraft did not enter orbit-->


<!--Spacecraft properties-->
<!--Spacecraft properties-->| spacecraft         = [[Polar Satellite Launch Vehicle]]
| spacecraft           = [[Polar Satellite Launch Vehicle]]
| spacecraft_type   = [[Launch vehicle]]
| spacecraft_type       = [[Launch vehicle]]
| spacecraft_bus     = <!--eg. A2100M, Star-2, etc-->
| spacecraft_bus       = <!--eg. A2100M, Star-2, etc-->
| manufacturer       = [[ISRO]] ([[Satellite Launch Vehicle|Launch Vehicle]]) &<br>[[Surrey Satellite Technology|Surrey Satellite]] ([[Satellite]]s)
| manufacturer         = [[ISRO]] ([[Satellite Launch Vehicle|Launch Vehicle]]) &<br>[[Surrey Satellite Technology|Surrey Satellite]] ([[Satellite]]s)
| launch_mass       = {{convert|320000|kg|lbs}}
| launch_mass           = {{convert|320000|kg|lbs}}
| BOL_mass           = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase-->
| BOL_mass             = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase-->
| landing_mass       = <!--Mass after landing (recovered spacecraft only)-->
| landing_mass         = <!--Mass after landing (recovered spacecraft only)-->
| dry_mass           = <!--spacecraft mass in orbit without fuel-->
| dry_mass             = <!--spacecraft mass in orbit without fuel-->
| payload_mass       = {{convert|1440|kg|lbs}}
| payload_mass         = {{convert|1440|kg|lbs}}
| dimensions         = <!--body dimensions and solar array span-->
| dimensions           = <!--body dimensions and solar array span-->
| power             = <!--end-of-life power, in watts-->
| power                 = <!--end-of-life power, in watts-->


<!--Expedition details-->
<!--Expedition details-->| space_station     = <!--space station the expedition occurred aboard-->
|space_station         = <!--space station the expedition occurred aboard-->
| start_date         = <!--date the crew took command of the station-->
|start_date             = <!--date the crew took command of the station-->
| end_date           = <!--date the crew ceased command of the station-->
|end_date               = <!--date the crew ceased command of the station-->
| arrival_craft     = <!--spacecraft the crew arrived aboard-->
|arrival_craft         = <!--spacecraft the crew arrived aboard-->
| departure_craft   = <!--spacecraft the crew departed aboard-->
|departure_craft       = <!--spacecraft the crew departed aboard-->


<!--Crew details-->
<!--Crew details-->| crew_size         = Nil
| crew_size             = Nil
| crew_members       = <!--crew who launched AND landed aboard the spacecraft-->
| crew_members         = <!--crew who launched AND landed aboard the spacecraft-->
| crew_launching     = <!--crew who only launched aboard the spacecraft-->
| crew_launching       = <!--crew who only launched aboard the spacecraft-->
| crew_landing       = <!--crew who only landed aboard the spacecraft-->
| crew_landing         = <!--crew who only landed aboard the spacecraft-->
| crew_callsign     = <!--spacecraft's callsign-->
| crew_callsign         = <!--spacecraft's callsign-->
| crew_expedition   = <!--space station expedition(s) the mission was in support of, do NOT use if the mission is an expedition itself-->
| crew_expedition       = <!--space station expedition(s) the mission was in support of, do NOT use if the mission is an expedition itself-->
| crew_EVAs         = <!--number of EVAs conducted during the mission-->
| crew_EVAs             = <!--number of EVAs conducted during the mission-->
| crew_EVA_duration = <!--time spent on EVA-->
| crew_EVA_duration     = <!--time spent on EVA-->
| crew_photo         = <!--omit the "file" prefix-->
| crew_photo           = <!--omit the "file" prefix-->
| crew_photo_alt     = <!--alt text for image-->
| crew_photo_alt       = <!--alt text for image-->
| crew_photo_caption = <!--image caption-->
| crew_photo_caption   = <!--image caption-->
| crew_photo_size   = <!--defaults to 220px-->
| crew_photo_size       = <!--defaults to 220px-->


<!--Launch details-->
<!--Launch details-->| launch_date       = {{start date|2015|07|10|21|58|00}} ([[Indian Standard Time|IST]])
| launch_date           = {{start date|2015|07|10|21|58|00|7=Z}} ([[Indian Standard Time|IST]])
| launch_rocket     = [[PSLV]]
| launch_rocket         = [[PSLV]]
| launch_site       = [[Satish Dhawan Space Centre]]
| launch_site           = [[Satish Dhawan Space Centre]]
| launch_contractor = [[ISRO]]
| launch_contractor     = [[ISRO]]
| deployment_from   = <!--place where deployed from-->
| deployment_from       = <!--place where deployed from-->
| deployment_date   = 10 Jul 2015
| deployment_date       = 10 Jul 2015
| entered_service   = <!--date on which the spacecraft entered service, if it did not do so immediately after launch-->
| entered_service       = <!--date on which the spacecraft entered service, if it did not do so immediately after launch-->
<!-- * - e.g. Proton-M/Briz-M not Proton-M, but Titan IV(401)A not Titan IV(401)A-Centaur-->
<!-- * - e.g. Proton-M/Briz-M not Proton-M, but Titan IV(401)A not Titan IV(401)A-Centaur-->


<!--end of mission-->
<!--end of mission-->| disposal_type     = Placed in [[graveyard orbit]]
| disposal_type         = Placed in [[graveyard orbit]]
| deactivated       = 10 Jul 2015
| deactivated           = 10 Jul 2015
| destroyed         = <!--when craft was destroyed (if other than by re-entry)-->
| destroyed             = <!--when craft was destroyed (if other than by re-entry)-->
| last_contact       = <!--when last signal received if not decommissioned-->
| last_contact         = <!--when last signal received if not decommissioned-->
| recovery_by       = <!--recovered by-->
| recovery_by           = <!--recovered by-->
| recovery_date     = <!--recovery date-->
| recovery_date         = <!--recovery date-->
| decay_date         = <!--when craft re-entered the atmosphere, not needed if it landed-->
| decay_date           = <!--when craft re-entered the atmosphere, not needed if it landed-->
| landing_date       = <!--when the spacecraft made a controlled landing, not needed if it did not return intact-->
| landing_date         = <!--when the spacecraft made a controlled landing, not needed if it did not return intact-->
| landing_site       = <!--where the craft landed; site/runway or coordinates-->
| landing_site         = <!--where the craft landed; site/runway or coordinates-->


<!--orbit parameters-->
<!--orbit parameters-->
<!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values-->
<!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values-->| orbit_reference   =  
| orbit_reference       =
| orbit_regime       = [[Sun-synchronous orbit]]
| orbit_regime         = [[Sun-synchronous orbit]]
| orbit_longitude   = <!--geosynchronous satellites only-->
| orbit_longitude       = <!--geosynchronous satellites only-->
| orbit_slot         = <!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)-->
| orbit_slot           = <!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)-->
| orbit_semimajor   = <!--semimajor axis-->
| orbit_semimajor       = <!--semimajor axis-->
| orbit_eccentricity = <!--orbital eccentricity-->
| orbit_eccentricity   = <!--orbital eccentricity-->
| orbit_periapsis   = <!--periapsis altitude-->
| orbit_periapsis       = <!--periapsis altitude-->  
| orbit_apoapsis     = <!--apoapsis altitude-->
| orbit_apoapsis       = <!--apoapsis altitude-->  
| orbit_inclination = <!--orbital inclination-->
| orbit_inclination     = <!--orbital inclination-->  
| orbit_period       = <!--time taken to complete an orbit-->
| orbit_period         = <!--time taken to complete an orbit-->
| orbit_RAAN         = <!--right ascension of the ascending node-->
| orbit_RAAN           = <!--right ascension of the ascending node-->
| orbit_arg_periapsis = <!--argument of perigee/periapsis-->
| orbit_arg_periapsis   = <!--argument of perigee/periapsis-->
| orbit_mean_anomaly = <!--mean anomaly at epoch, only use in conjunction with an epoch value-->
| orbit_mean_anomaly   = <!--mean anomaly at epoch, only use in conjunction with an epoch value-->
| orbit_mean_motion = <!--mean motion of the satellite, usually measured in orbits per day-->
| orbit_mean_motion     = <!--mean motion of the satellite, usually measured in orbits per day-->
| orbit_repeat       = <!--repeat interval/revisit time-->
| orbit_repeat         = <!--repeat interval/revisit time-->
| orbit_velocity     = <!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity-->
| orbit_velocity       = <!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity-->
| orbit_epoch       = <!--the date at which the orbit parameters were correct-->
| orbit_epoch           = <!--the date at which the orbit parameters were correct-->
| orbit_rev_number   = <!--revolution number-->
| orbit_rev_number     = <!--revolution number-->
| apsis             = <!--planet specific apsis term (eg. gee/helion/selene/etc - defaults to generic "apsis")-->
| apsis                 = <!--planet specific apsis term (eg. gee/helion/selene/etc - defaults to generic "apsis")-->
| interplanetary     = <!--Infobox spaceflight/IP can be called multiple times for missions with multiple targets or combined orbiter/lander missions, etc-->
|interplanetary         = <!--Infobox spaceflight/IP can be called multiple times for missions with multiple targets or combined orbiter/lander missions, etc-->


<!--Cargo parameters-->
<!--Cargo parameters-->| payload_items     = Three DMC3 satellites,<br>One CBNT-1 (technology demonstrator)&,<br>One De-OrbitSail (TD nano satellite)
| payload_items         = Three DMC3 satellites,<br>One CBNT-1 (technology demonstrator)&,<br>One De-OrbitSail (TD nano satellite)
| cargo_mass         = <!--Mass of the cargo aboard-->
| cargo_mass           = <!--Mass of the cargo aboard-->
| cargo_mass_press   = <!--Mass of pressurised cargo-->
| cargo_mass_press     = <!--Mass of pressurised cargo-->
| cargo_mass_unpress = <!--Mass of unpressurised cargo (e.g. Dragon Trunk)-->
| cargo_mass_unpress   = <!--Mass of unpressurised cargo (e.g. Dragon Trunk)-->
| cargo_mass_fuel   = <!--Mass of fuel transferred from spacecraft's tanks-->
| cargo_mass_fuel       = <!--Mass of fuel transferred from spacecraft's tanks-->
| cargo_mass_gas     = <!--Mass of gasses transferred (e.g. oxygen)-->
| cargo_mass_gas       = <!--Mass of gasses transferred (e.g. oxygen)-->
| cargo_mass_water   = <!--Mass of water transferred-->
| cargo_mass_water     = <!--Mass of water transferred-->


<!--Telescope parameters-->
<!--Telescope parameters-->| instrument_type   = <!--converts telescope fields to suit a camera or other similar instrument-->
| instrument_type       = <!--converts telescope fields to suit a camera or other similar instrument-->
| telescope_name     = <!--name, if different to the satellite-->
| telescope_name       = <!--name, if different to the satellite-->
| telescope_type     = <!--type of telescope, mirror arrangement, etc-->
| telescope_type       = <!--type of telescope, mirror arrangement, etc-->  
| telescope_diameter = <!--diameter of telescope-->
| telescope_diameter   = <!--diameter of telescope-->
| telescope_focal_length = <!--focal length of telescope-->
| telescope_focal_length= <!--focal length of telescope-->
| telescope_area     = <!--collecting area-->
| telescope_area       = <!--collecting area-->
| telescope_wavelength = <!--wavelengths at which the telescope operates-->
| telescope_wavelength = <!--wavelengths at which the telescope operates-->  
| telescope_resolution = <!--resolution of telescope-->
| telescope_resolution = <!--resolution of telescope-->
| instruments       = <!--a list of instruments on the satellite-->
| instruments           = <!--a list of instruments on the satellite-->


<!--transponder parameters-->
<!--transponder parameters-->| trans_band         = <!--Transponder frequency bands-->
| trans_band           = <!--Transponder frequency bands-->
| trans_frequency   = <!--specific frequencies-->
| trans_frequency       = <!--specific frequencies-->
| trans_bandwidth   = <!--bandwidth-->
| trans_bandwidth       = <!--bandwidth-->
| trans_capacity     = <!--capacity of the transponders-->
| trans_capacity       = <!--capacity of the transponders-->
| trans_coverage     = <!--area covered-->
| trans_coverage       = <!--area covered-->
| trans_TWTA         = <!--TWTA output power-->
| trans_TWTA           = <!--TWTA output power-->
| trans_EIRP         = <!--equivalent isotropic power-->
| trans_EIRP           = <!--equivalent isotropic power-->
| trans_HPBW         = <!--half-power beam width-->
| trans_HPBW           = <!--half-power beam width-->


<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions.  
<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions.  
If in doubt, leave it out-->
If in doubt, leave it out-->| programme         = '''[[Polar Satellite Launch Vehicle#Launch history|Polar Satellite Launch Vehicle missions]]'''
| programme             = '''[[Polar Satellite Launch Vehicle#Launch history|Polar Satellite Launch Vehicle missions]]'''
| previous_mission   = '''PSLV-C27'''
| previous_mission     = '''PSLV-C27'''
| next_mission       = '''PSLV-C29'''
| next_mission         = '''PSLV-C29'''


<!--mission insignia or patch-->
<!--mission insignia or patch-->| insignia           = <!--omit the "file" prefix-->
| insignia             = <!--omit the "file" prefix-->
| insignia_caption   = <!--image caption-->
| insignia_caption     = <!--image caption-->
| insignia_alt       = <!--image alt text-->
| insignia_alt         = <!--image alt text-->
| insignia_size     = <!--include px/em; defaults to 180px-->
| insignia_size         = <!--include px/em; defaults to 180px-->
}}
}}
'''PSLV-C28''' ([[Pseudonym|a.k.a.]] ''DMC3 mission'') was the 29th consecutive successful mission (overall 30th) of the [[PSLV]] program. The PSLV-C28 carried and successfully deployed 5 [[satellite]]s in the [[Sun-synchronous orbit]]. With a launch mass of {{convert|320000|kg|lbs}} and payload mass of payload mass {{convert|1440|kg|lbs}}, the C28 was the heaviest commercial mission undertaken by the [[Indian Space Research Organisation]] and [[Antrix Corporation]]. The PSLV-C28 carried three identical optical [[earth observation satellite]]s ([[UK-DMC 3|DMC3-1]], DMC3-2 & DMC3-3), an optical [[earth observation]] [[technology demonstration|technology demonstrator]] [[Miniaturized satellite|microsatellite]] (CBNT-1), and an experimental [[Nano Satellites|nanosatellite]] (De-orbitSail). All the satellites were built by [[Surrey Satellite Technology]] (SSTL). Although built by SSTL, the "De-orbitSail" belonged to the Surrey Space Centre.<ref name="PSLV-C28 / DMC3 Mission">{{cite news|title=PSLV-C28 / DMC3 Mission|publisher=[[ISRO]] website|accessdate=7 Jun 2016|url=http://www.isro.gov.in/launcher/pslv-c28-dmc3-mission}}</ref><ref name="Polar Satellite Launch Vehicle">{{cite news|title=Polar Satellite Launch Vehicle|publisher=[[Vikram Sarabhai Space Centre]] website|accessdate=7 Jun 2016|url=http://www.vssc.gov.in/VSSC_V4/index.php/launchers/launchers-pslv}}</ref><ref name="DMC 3-FM3">{{cite news|title=DMC 3-FM3|publisher=[[NASA]] website|accessdate=7 Jun 2016|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2015-032C}}</ref><ref name="Carbonite 1">{{cite news|title=Carbonite 1|publisher=[[NASA]] website|accessdate=7 Jun 2016|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2015-032D}}</ref><ref name="ISRO successfully Launches PSLV-C28 carrying 5 UK satellites">{{cite news|title=ISRO successfully Launches PSLV-C28 carrying 5 UK satellites|work=[[The Times of India]]|accessdate=7 Jun 2016|url=http://timesofindia.indiatimes.com/india/Isro-successfully-launches-PSLV-C28-carrying-5-UK-satellites/articleshow/48023816.cms}}</ref><ref name="10 things you should know about PSLV-C28">{{cite news|title=10 things you should know about PSLV-C28|publisher=scoopwhoop.com|accessdate=7 Jun 2016|url=http://www.scoopwhoop.com/inothernews/isro-pslv-c28-satellite-launch/}}</ref>
'''PSLV-C28''' ([[Pseudonym|a.k.a.]] ''DMC3 mission'') was the 29th consecutive successful mission (overall 30th) of the [[PSLV]] program. The PSLV-C28 carried and successfully deployed 5 [[satellite]]s in the [[Sun-synchronous orbit]]. With a launch mass of {{convert|320000|kg|lbs}} and payload mass of payload mass {{convert|1440|kg|lbs}}, the C28 was the heaviest commercial mission undertaken by the [[Indian Space Research Organisation]] and [[Antrix Corporation]]. The PSLV-C28 carried three identical optical [[Earth observation satellite]]s ([[UK-DMC 3|DMC3-1]], DMC3-2 & DMC3-3), an optical [[Earth observation]] [[technology demonstration|technology demonstrator]] [[Miniaturized satellite|microsatellite]] (CBNT-1), and an experimental [[Nano Satellites|nanosatellite]] (De-orbitSail). All the satellites were built by [[Surrey Satellite Technology]] (SSTL). Although built by SSTL, the "De-orbitSail" belonged to the Surrey Space Centre.<ref name="PSLV-C28 / DMC3 Mission">{{cite news|title=PSLV-C28 / DMC3 Mission|publisher=[[ISRO]] website|accessdate=7 Jun 2016|url=http://www.isro.gov.in/launcher/pslv-c28-dmc3-mission|archive-date=29 September 2015|archive-url=https://web.archive.org/web/20150929042503/http://www.isro.gov.in/launcher/pslv-c28-dmc3-mission|url-status=dead}}</ref><ref name="Polar Satellite Launch Vehicle">{{cite news|title=Polar Satellite Launch Vehicle|publisher=[[Vikram Sarabhai Space Centre]] website|accessdate=7 Jun 2016|url=http://www.vssc.gov.in/VSSC_V4/index.php/launchers/launchers-pslv}}</ref><ref name="DMC 3-FM3">{{cite news|title=DMC 3-FM3|publisher=[[NASA]] website|accessdate=7 Jun 2016|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2015-032C}}</ref><ref name="Carbonite 1">{{cite news|title=Carbonite 1|publisher=[[NASA]] website|accessdate=7 Jun 2016|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2015-032D}}</ref><ref name="ISRO successfully Launches PSLV-C28 carrying 5 UK satellites">{{cite news|title=ISRO successfully Launches PSLV-C28 carrying 5 UK satellites|work=[[The Times of India]]|accessdate=7 Jun 2016|url=http://timesofindia.indiatimes.com/india/Isro-successfully-launches-PSLV-C28-carrying-5-UK-satellites/articleshow/48023816.cms}}</ref><ref name="10 things you should know about PSLV-C28">{{cite news|title=10 things you should know about PSLV-C28|publisher=scoopwhoop.com|accessdate=7 Jun 2016|url=http://www.scoopwhoop.com/inothernews/isro-pslv-c28-satellite-launch/}}</ref>


==See also==
==See also==

Latest revision as of 18:06, 11 March 2026

"DMC 3" redirects here. For the 2005 video game, see Devil May Cry 3: Dante's Awakening.
PSLV-C28
Model of the PSLV rocket
Mission typeDeployment of 5 satellites.
OperatorISRO & Antrix Corporation
COSPAR ID2015-032C & 2015-032D
SATCAT no.40717 & 40718
WebsiteISRO website
Mission duration19 minutes & 21 seconds
Distance travelled647 km
Spacecraft properties
SpacecraftPolar Satellite Launch Vehicle
Spacecraft typeLaunch vehicle
ManufacturerISRO (Launch Vehicle) &
Surrey Satellite (Satellites)
Launch mass320,000 kilograms (710,000 lb)
Payload mass1,440 kilograms (3,170 lb)
Start of mission
Launch date21:58:00, July 10, 2015 (2015-07-10T21:58:00) (IST)
RocketPSLV
Launch siteSatish Dhawan Space Centre
ContractorISRO
Deployment date10 Jul 2015
End of mission
DisposalPlaced in graveyard orbit
Deactivated10 Jul 2015
Orbital parameters
RegimeSun-synchronous orbit
Payload
Three DMC3 satellites,
One CBNT-1 (technology demonstrator)&,
One De-OrbitSail (TD nano satellite)
← PSLV-C27
PSLV-C29 →
 

PSLV-C28 (a.k.a. DMC3 mission) was the 29th consecutive successful mission (overall 30th) of the PSLV program. The PSLV-C28 carried and successfully deployed 5 satellites in the Sun-synchronous orbit. With a launch mass of 320,000 kilograms (710,000 lb) and payload mass of payload mass 1,440 kilograms (3,170 lb), the C28 was the heaviest commercial mission undertaken by the Indian Space Research Organisation and Antrix Corporation. The PSLV-C28 carried three identical optical Earth observation satellites (DMC3-1, DMC3-2 & DMC3-3), an optical Earth observation technology demonstrator microsatellite (CBNT-1), and an experimental nanosatellite (De-orbitSail). All the satellites were built by Surrey Satellite Technology (SSTL). Although built by SSTL, the "De-orbitSail" belonged to the Surrey Space Centre.[1][2][3][4][5][6]

See also[edit | edit source]

References[edit | edit source]

  1. ↑ "PSLV-C28 / DMC3 Mission". ISRO website. Archived from the original on 29 September 2015. Retrieved 7 Jun 2016.
  2. ↑ "Polar Satellite Launch Vehicle". Vikram Sarabhai Space Centre website. Retrieved 7 Jun 2016.
  3. ↑ "DMC 3-FM3". NASA website. Retrieved 7 Jun 2016.
  4. ↑ "Carbonite 1". NASA website. Retrieved 7 Jun 2016.
  5. ↑ "ISRO successfully Launches PSLV-C28 carrying 5 UK satellites". The Times of India. Retrieved 7 Jun 2016.
  6. ↑ "10 things you should know about PSLV-C28". scoopwhoop.com. Retrieved 7 Jun 2016.
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