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{{Infobox spaceflight | {{Infobox spaceflight | ||
| name | | name = PSLV-D3 | ||
<!--image of the spacecraft/mission--> | <!--image of the spacecraft/mission-->| image = PSLV.svg | ||
| image | | image_caption = Model of the [[PSLV]] rocket | ||
| image_caption | | image_alt = <!--image alt text--> | ||
| image_alt | | image_size = 70px | ||
| image_size | <!--Basic details-->| mission_type = Deployment of one [[satellite]]. | ||
<!--Basic details--> | | operator = [[ISRO]] | ||
| mission_type | | Harvard_designation = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)--> | ||
| operator | | COSPAR_ID = | ||
| Harvard_designation | | SATCAT = | ||
| COSPAR_ID | | website = [http://www.isro.gov.in/ ISRO website] | ||
| SATCAT | | mission_duration = | ||
| website | | distance_travelled = | ||
| mission_duration | | orbits_completed = <!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit--> | ||
| distance_travelled | | suborbital_range = <!--downrange distance reached if spacecraft did not enter orbit--> | ||
| orbits_completed | | suborbital_apogee = <!--altitude reached if spacecraft did not enter orbit--> | ||
| suborbital_range | |||
| suborbital_apogee | |||
<!--Spacecraft properties--> | <!--Spacecraft properties-->| spacecraft = [[Polar Satellite Launch Vehicle]] | ||
| spacecraft | | spacecraft_type = [[Launch vehicle]] | ||
| spacecraft_type | | spacecraft_bus = <!--eg. A2100M, Star-2, etc--> | ||
| spacecraft_bus | | manufacturer = [[ISRO]] | ||
| manufacturer | | launch_mass = {{convert|295000|kg|lbs}} | ||
| launch_mass | | BOL_mass = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase--> | ||
| BOL_mass | | landing_mass = <!--Mass after landing (recovered spacecraft only)--> | ||
| landing_mass | | dry_mass = <!--spacecraft mass in orbit without fuel--> | ||
| dry_mass | | payload_mass = {{convert|920|kg|lbs}} | ||
| payload_mass | | dimensions = <!--body dimensions and solar array span--> | ||
| dimensions | | power = <!--end-of-life power, in watts--> | ||
| power | |||
<!--Expedition details--> | <!--Expedition details-->| space_station = <!--space station the expedition occurred aboard--> | ||
|space_station | | start_date = <!--date the crew took command of the station--> | ||
|start_date | | end_date = <!--date the crew ceased command of the station--> | ||
|end_date | | arrival_craft = <!--spacecraft the crew arrived aboard--> | ||
|arrival_craft | | departure_craft = <!--spacecraft the crew departed aboard--> | ||
|departure_craft | |||
<!--Crew details--> | <!--Crew details-->| crew_size = Nil | ||
| crew_size | | crew_members = <!--crew who launched AND landed aboard the spacecraft--> | ||
| crew_members | | crew_launching = <!--crew who only launched aboard the spacecraft--> | ||
| crew_launching | | crew_landing = <!--crew who only landed aboard the spacecraft--> | ||
| crew_landing | | crew_callsign = <!--spacecraft's callsign--> | ||
| crew_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 | | crew_EVAs = <!--number of EVAs conducted during the mission--> | ||
| crew_EVAs | | crew_EVA_duration = <!--time spent on EVA--> | ||
| crew_EVA_duration | | crew_photo = <!--omit the "file" prefix--> | ||
| crew_photo | | crew_photo_alt = <!--alt text for image--> | ||
| crew_photo_alt | | crew_photo_caption = <!--image caption--> | ||
| crew_photo_caption | | crew_photo_size = <!--defaults to 220px--> | ||
| crew_photo_size | |||
<!--Launch details--> | <!--Launch details-->| launch_date = {{start date|1996|03|21|04|53|00}} ([[Indian Standard Time|IST]]) | ||
| launch_date | | launch_rocket = [[PSLV]] | ||
| launch_rocket | | launch_site = [[Satish Dhawan Space Centre|Sriharikota Launching Range]] | ||
| launch_site | | launch_contractor = [[ISRO]] | ||
| launch_contractor | | deployment_from = <!--place where deployed from--> | ||
| deployment_from | | deployment_date = | ||
| deployment_date | | entered_service = <!--date on which the spacecraft entered service, if it did not do so immediately after launch--> | ||
| entered_service | |||
<!-- * - 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 | | deactivated = 21 March 1996 | ||
| deactivated | | destroyed = <!--when craft was destroyed (if other than by re-entry)--> | ||
| destroyed | | last_contact = <!--when last signal received if not decommissioned--> | ||
| last_contact | | recovery_by = <!--recovered by--> | ||
| recovery_by | | recovery_date = <!--recovery date--> | ||
| recovery_date | | decay_date = <!--when craft re-entered the atmosphere, not needed if it landed--> | ||
| decay_date | | landing_date = <!--when the spacecraft made a controlled landing, not needed if it did not return intact--> | ||
| landing_date | | landing_site = <!--where the craft landed; site/runway or coordinates--> | ||
| landing_site | |||
<!--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|Sun-synchronous]] [[Low Earth orbit]] | ||
| orbit_regime | | orbit_longitude = <!--geosynchronous satellites only--> | ||
| orbit_longitude | | orbit_slot = <!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)--> | ||
| orbit_slot | | orbit_semimajor = <!--semimajor axis--> | ||
| orbit_semimajor | | orbit_eccentricity = <!--orbital eccentricity--> | ||
| orbit_eccentricity | | orbit_periapsis = <!--periapsis altitude--> | ||
| orbit_periapsis | | orbit_apoapsis = <!--apoapsis altitude--> | ||
| orbit_apoapsis | | orbit_inclination = <!--orbital inclination--> | ||
| orbit_inclination | | orbit_period = <!--time taken to complete an orbit--> | ||
| orbit_period | | orbit_RAAN = <!--right ascension of the ascending node--> | ||
| orbit_RAAN | | orbit_arg_periapsis = <!--argument of perigee/periapsis--> | ||
| orbit_arg_periapsis | | orbit_mean_anomaly = <!--mean anomaly at epoch, only use in conjunction with an epoch value--> | ||
| orbit_mean_anomaly | | orbit_mean_motion = <!--mean motion of the satellite, usually measured in orbits per day--> | ||
| orbit_mean_motion | | orbit_repeat = <!--repeat interval/revisit time--> | ||
| orbit_repeat | | orbit_velocity = <!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity--> | ||
| orbit_velocity | | orbit_epoch = <!--the date at which the orbit parameters were correct--> | ||
| orbit_epoch | | orbit_rev_number = <!--revolution number--> | ||
| orbit_rev_number | | apsis = <!--planet specific apsis term (eg. gee/helion/selene/etc - defaults to generic "apsis")--> | ||
| apsis | | interplanetary = <!--Infobox spaceflight/IP can be called multiple times for missions with multiple targets or combined orbiter/lander missions, etc--> | ||
|interplanetary | |||
<!--Cargo parameters--> | <!--Cargo parameters-->| payload_items = [[IRS-P3]] | ||
| payload_items | | cargo_mass = <!--Mass of the cargo aboard--> | ||
| cargo_mass | | cargo_mass_press = <!--Mass of pressurised cargo--> | ||
| cargo_mass_press | | cargo_mass_unpress = <!--Mass of unpressurised cargo (e.g. Dragon Trunk)--> | ||
| cargo_mass_unpress | | cargo_mass_fuel = <!--Mass of fuel transferred from spacecraft's tanks--> | ||
| cargo_mass_fuel | | cargo_mass_gas = <!--Mass of gasses transferred (e.g. oxygen)--> | ||
| cargo_mass_gas | | cargo_mass_water = <!--Mass of water transferred--> | ||
| cargo_mass_water | |||
<!--Telescope parameters--> | <!--Telescope parameters-->| instrument_type = <!--converts telescope fields to suit a camera or other similar instrument--> | ||
| instrument_type | | telescope_name = <!--name, if different to the satellite--> | ||
| telescope_name | | telescope_type = <!--type of telescope, mirror arrangement, etc--> | ||
| telescope_type | | telescope_diameter = <!--diameter of telescope--> | ||
| telescope_diameter | | telescope_focal_length = <!--focal length of telescope--> | ||
| telescope_focal_length= <!--focal length of telescope--> | | telescope_area = <!--collecting area--> | ||
| telescope_area | | telescope_wavelength = <!--wavelengths at which the telescope operates--> | ||
| telescope_wavelength | | telescope_resolution = <!--resolution of telescope--> | ||
| telescope_resolution | | instruments = <!--a list of instruments on the satellite--> | ||
| instruments | |||
<!--transponder parameters--> | <!--transponder parameters-->| trans_band = <!--Transponder frequency bands--> | ||
| trans_band | | trans_frequency = <!--specific frequencies--> | ||
| trans_frequency | | trans_bandwidth = <!--bandwidth--> | ||
| trans_bandwidth | | trans_capacity = <!--capacity of the transponders--> | ||
| trans_capacity | | trans_coverage = <!--area covered--> | ||
| trans_coverage | | trans_TWTA = <!--TWTA output power--> | ||
| trans_TWTA | | trans_EIRP = <!--equivalent isotropic power--> | ||
| trans_EIRP | | trans_HPBW = <!--half-power beam width--> | ||
| trans_HPBW | |||
<!--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 | | previous_mission = '''[[PSLV-D2]]''' | ||
| previous_mission | | next_mission = '''[[PSLV-C1]]''' | ||
| next_mission | |||
<!--mission insignia or patch--> | <!--mission insignia or patch-->| insignia = <!--omit the "file" prefix--> | ||
| insignia | | insignia_caption = <!--image caption--> | ||
| insignia_caption | | insignia_alt = <!--image alt text--> | ||
| insignia_alt | | insignia_size = <!--include px/em; defaults to 180px--> | ||
| insignia_size | |||
}} | }} | ||
'''PSLV-D3''' was the overall third and second successful mission of the [[PSLV]] program by [[Indian Space Research Organisation]]. The vehicle carried [[IRS-P3]] satellite which was deployed in the [[Sun-synchronous orbit|Sun-synchronous]] [[Low Earth orbit]].<ref name="PSLV-D3">{{cite news|title=PSLV-D3|publisher=[[Indian Space Research Organisation]] website|accessdate=23 Jun 2016|url=http://www.isro.gov.in/launcher/pslv-d3}}</ref><ref name="PSLV Launch Vehicle">{{cite news|title=PSLV Launch Vehicle|publisher=spaceflight101.com|accessdate=23 Jun 2016|url=http://spaceflight101.com/spacerockets/pslv/}}</ref><ref name="PSLV">{{cite news|title=PSLV|publisher=spacelaunchreport.com|accessdate=23 Jun 2016|url=http://www.spacelaunchreport.com/pslv.html}}</ref><ref name="ISRO Timeline">{{cite news|title=ISRO Timeline|publisher=[[Indian Space Research Organisation]] website|accessdate=23 Jun 2016|url=http://www.isro.gov.in/about-isro/isros-timeline-1960s-to-today#33}}</ref> | '''PSLV-D3''' was the overall third and second successful mission of the [[PSLV]] program by [[Indian Space Research Organisation]]. The vehicle carried [[IRS-P3]] satellite which was deployed in the [[Sun-synchronous orbit|Sun-synchronous]] [[Low Earth orbit]].<ref name="PSLV-D3">{{cite news|title=PSLV-D3|publisher=[[Indian Space Research Organisation]] website|accessdate=23 Jun 2016|url=http://www.isro.gov.in/launcher/pslv-d3|archive-date=11 August 2016|archive-url=https://web.archive.org/web/20160811040311/http://www.isro.gov.in/launcher/pslv-d3|url-status=dead}}</ref><ref name="PSLV Launch Vehicle">{{cite news|title=PSLV Launch Vehicle|publisher=spaceflight101.com|accessdate=23 Jun 2016|url=http://spaceflight101.com/spacerockets/pslv/|archive-date=28 June 2016|archive-url=https://web.archive.org/web/20160628060239/http://spaceflight101.com/spacerockets/pslv|url-status=dead}}</ref><ref name="PSLV">{{cite news|title=PSLV|publisher=spacelaunchreport.com|accessdate=23 Jun 2016|url=http://www.spacelaunchreport.com/pslv.html|archive-url=https://archive.today/20130104225437/http://www.spacelaunchreport.com/pslv.html|url-status=usurped|archive-date=January 4, 2013}}</ref><ref name="ISRO Timeline">{{cite news|title=ISRO Timeline|publisher=[[Indian Space Research Organisation]] website|accessdate=23 Jun 2016|url=http://www.isro.gov.in/about-isro/isros-timeline-1960s-to-today#33|archive-date=20 November 2016|archive-url=https://web.archive.org/web/20161120150630/http://isro.gov.in/about-isro/isros-timeline-1960s-to-today#33|url-status=dead}}</ref> | ||
==Launch== | ==Launch== | ||
PSLV-D3 was launched at 4:53 a.m. [[Indian Standard Time|IST]] on 21 March 1996 from [[Satish Dhawan Space Centre]] (then called "Sriharikota Launching Range"). The vehicle successfully achieved orbit, placing the [[IRS-P3]] satellite in the [[ | PSLV-D3 was launched at 4:53 a.m. [[Indian Standard Time|IST]] on 21 March 1996 from [[Satish Dhawan Space Centre]] (then called "Sriharikota Launching Range"). The vehicle successfully achieved orbit, placing the [[IRS-P3]] satellite in the [[Sun-synchronous orbit]].<ref name="PSLV-D3"/><ref name="PSLV Launch Vehicle"/><ref name="PSLV"/><ref name="ISRO Timeline"/> | ||
==See also== | ==See also== | ||
Latest revision as of 09:02, 19 July 2025
Model of the PSLV rocket | |
| Mission type | Deployment of one satellite. |
|---|---|
| Operator | ISRO |
| COSPAR ID | {{#property:P247}} |
| Website | ISRO website |
| Spacecraft properties | |
| Spacecraft | Polar Satellite Launch Vehicle |
| Spacecraft type | Launch vehicle |
| Manufacturer | ISRO |
| Launch mass | 295,000 kilograms (650,000 lb) |
| Payload mass | 920 kilograms (2,030 lb) |
| Start of mission | |
| Launch date | 04:53:00, March 21, 1996 (IST) |
| Rocket | PSLV |
| Launch site | Sriharikota Launching Range |
| Contractor | ISRO |
| End of mission | |
| Disposal | Placed in graveyard orbit |
| Deactivated | 21 March 1996 |
| Orbital parameters | |
| Regime | Sun-synchronous Low Earth orbit |
| Payload | |
| IRS-P3 | |
PSLV-D3 was the overall third and second successful mission of the PSLV program by Indian Space Research Organisation. The vehicle carried IRS-P3 satellite which was deployed in the Sun-synchronous Low Earth orbit.[1][2][3][4]
Launch[edit | edit source]
PSLV-D3 was launched at 4:53 a.m. IST on 21 March 1996 from Satish Dhawan Space Centre (then called "Sriharikota Launching Range"). The vehicle successfully achieved orbit, placing the IRS-P3 satellite in the Sun-synchronous orbit.[1][2][3][4]
See also[edit | edit source]
References[edit | edit source]
- ↑ 1.0 1.1 "PSLV-D3". Indian Space Research Organisation website. Archived from the original on 11 August 2016. Retrieved 23 Jun 2016.
- ↑ 2.0 2.1 "PSLV Launch Vehicle". spaceflight101.com. Archived from the original on 28 June 2016. Retrieved 23 Jun 2016.
- ↑ 3.0 3.1 "PSLV". spacelaunchreport.com. Retrieved 23 Jun 2016.
{{cite news}}: CS1 maint: deprecated archival service (link) - ↑ 4.0 4.1 "ISRO Timeline". Indian Space Research Organisation website. Archived from the original on 20 November 2016. Retrieved 23 Jun 2016.