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		<title>Ajay Kumar: Created a new article</title>
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		<summary type="html">&lt;p&gt;Created a new article&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{Infobox spaceflight&lt;br /&gt;
| name                  = PSLV-C3&lt;br /&gt;
| names_list            = &amp;lt;!--list of previous names if the spacecraft has been renamed. &lt;br /&gt;
Include the dates applicable if possible, and separate each name with a linebreak. &lt;br /&gt;
Omit if the spacecraft has only ever been known by one name. &lt;br /&gt;
Do not include Harvard, COSPAR/NSSDC or SATCAT/NORAD/NASA designations as alternative names--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--image of the spacecraft/mission--&amp;gt;&lt;br /&gt;
| image                 = PSLV.svg&lt;br /&gt;
| image_caption         = Model of the [[PSLV]] rocket&lt;br /&gt;
| image_alt             = &amp;lt;!--image alt text--&amp;gt;&lt;br /&gt;
| image_size            = 70px&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Basic details--&amp;gt;&lt;br /&gt;
| mission_type          = Deployment of three [[satellite]]s.&lt;br /&gt;
| operator              =[[ISRO]]&lt;br /&gt;
| Harvard_designation   = &amp;lt;!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)--&amp;gt;&lt;br /&gt;
| COSPAR_ID             = &amp;lt;!--spacecraft launched since 1963 only (aka NSSDC ID; eg. 1998-067A)--&amp;gt;&lt;br /&gt;
| SATCAT                = &amp;lt;!--satellite catalogue number, omit leading zeroes (e.g. 25544)--&amp;gt;&lt;br /&gt;
| website               = [http://www.isro.gov.in/ ISRO website]&lt;br /&gt;
| mission_duration      = 1,658 seconds&lt;br /&gt;
| distance_travelled    = &amp;lt;!--How far the spacecraft travelled (if known)--&amp;gt;&lt;br /&gt;
| orbits_completed      = &amp;lt;!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit--&amp;gt;&lt;br /&gt;
| suborbital_range      = &amp;lt;!--downrange distance reached if spacecraft did not enter orbit--&amp;gt;&lt;br /&gt;
| suborbital_apogee     = {{convert|586.7|km|mi|0}}&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Spacecraft properties--&amp;gt;&lt;br /&gt;
| spacecraft            = [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
| spacecraft_type       = [[Expendable launch vehicle]]&lt;br /&gt;
| spacecraft_bus        = &amp;lt;!--eg. A2100M, Star-2, etc--&amp;gt;&lt;br /&gt;
| manufacturer          =[[ISRO]]&lt;br /&gt;
| launch_mass           = {{convert|294000|kg|lbs}}&lt;br /&gt;
| BOL_mass              = &amp;lt;!--spacecraft mass in orbit at beginning of operational life, after LEOP phase--&amp;gt;&lt;br /&gt;
| landing_mass          = &amp;lt;!--Mass after landing (recovered spacecraft only)--&amp;gt;&lt;br /&gt;
| dry_mass              = &amp;lt;!--spacecraft mass in orbit without fuel--&amp;gt;&lt;br /&gt;
| payload_mass          = {{convert|1294|kg|lbs}}&lt;br /&gt;
| dimensions            = {{convert|44.4|m|ft|0}}&amp;lt;br&amp;gt;(overall height)&lt;br /&gt;
| power                 = &amp;lt;!--end-of-life power, in watts--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Expedition details--&amp;gt;&lt;br /&gt;
|space_station          = &amp;lt;!--space station the expedition occurred aboard--&amp;gt;&lt;br /&gt;
|start_date             = &amp;lt;!--date the crew took command of the station--&amp;gt;&lt;br /&gt;
|end_date               = &amp;lt;!--date the crew ceased command of the station--&amp;gt;&lt;br /&gt;
|arrival_craft          = &amp;lt;!--spacecraft the crew arrived aboard--&amp;gt;&lt;br /&gt;
|departure_craft        = &amp;lt;!--spacecraft the crew departed aboard--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Launch details--&amp;gt;&lt;br /&gt;
| launch_date           = {{start date|2001|10|22|10|23|00|7=IST}} ([[Indian Standard Time|IST]])&lt;br /&gt;
| launch_rocket         = [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
| launch_site           = [[Satish Dhawan Space Centre|Sriharikota Launching Range]]&lt;br /&gt;
| launch_contractor     =[[ISRO]]&lt;br /&gt;
| deployment_from       = &amp;lt;!--place where deployed from--&amp;gt;&lt;br /&gt;
| deployment_date       = &amp;lt;!--date deployed--&amp;gt;&lt;br /&gt;
| entered_service       = &amp;lt;!--date on which the spacecraft entered service, if it did not do so immediately after launch--&amp;gt;&lt;br /&gt;
&amp;lt;!-- * - e.g. Proton-M/Briz-M not Proton-M, but Titan IV(401)A not Titan IV(401)A-Centaur--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--end of mission--&amp;gt;&lt;br /&gt;
| disposal_type         = Placed in [[graveyard orbit]]&lt;br /&gt;
| deactivated           = {{end date|2001|10|22}}&lt;br /&gt;
| destroyed             = &amp;lt;!--when craft was destroyed (if other than by re-entry)--&amp;gt;&lt;br /&gt;
| last_contact          = &amp;lt;!--when last signal received if not decommissioned--&amp;gt;&lt;br /&gt;
| recovery_by           = &amp;lt;!--recovered by--&amp;gt;&lt;br /&gt;
| recovery_date         = &amp;lt;!--recovery date--&amp;gt;&lt;br /&gt;
| decay_date            = &amp;lt;!--when craft re-entered the atmosphere, not needed if it landed--&amp;gt;&lt;br /&gt;
| landing_date          = &amp;lt;!--when the spacecraft made a controlled landing, not needed if it did not return intact--&amp;gt;&lt;br /&gt;
| landing_site          = &amp;lt;!--where the craft landed; site/runway or coordinates--&amp;gt;&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
    The following template should be used for ONE of the three above fields &amp;quot;end_of_mission&amp;quot;, &amp;quot;decay&amp;quot; or &amp;quot;landing&amp;quot; if the spacecraft is no longer operational.&lt;br /&gt;
    If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered.&lt;br /&gt;
    {{end date|YYYY|MM|DD|hh|mm|ss|TZ=Z}} (for Zulu/UTC) or {{end date|YYYY|MM|DD}} (if time unknown) &lt;br /&gt;
--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--orbit parameters--&amp;gt;&lt;br /&gt;
&amp;lt;!--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--&amp;gt;&lt;br /&gt;
| orbit_reference       = [[Sun-synchronous orbit|Sun-synchronous]] &lt;br /&gt;
| orbit_regime          = [[Low Earth orbit]]&lt;br /&gt;
| orbit_longitude       = &amp;lt;!--geosynchronous satellites only--&amp;gt;&lt;br /&gt;
| orbit_slot            = &amp;lt;!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)--&amp;gt;&lt;br /&gt;
| orbit_semimajor       = &amp;lt;!--semimajor axis--&amp;gt;&lt;br /&gt;
| orbit_eccentricity    = &amp;lt;!--orbital eccentricity--&amp;gt;&lt;br /&gt;
| orbit_periapsis       = &amp;lt;!--periapsis altitude--&amp;gt; &lt;br /&gt;
| orbit_apoapsis        = &amp;lt;!--apoapsis altitude--&amp;gt; &lt;br /&gt;
| orbit_inclination     = &amp;lt;!--orbital inclination--&amp;gt;  &lt;br /&gt;
| orbit_period          = &amp;lt;!--time taken to complete an orbit--&amp;gt;&lt;br /&gt;
| orbit_RAAN            = &amp;lt;!--right ascension of the ascending node--&amp;gt;&lt;br /&gt;
| orbit_arg_periapsis   = &amp;lt;!--argument of perigee/periapsis--&amp;gt;&lt;br /&gt;
| orbit_mean_anomaly    = &amp;lt;!--mean anomaly at epoch, only use in conjunction with an epoch value--&amp;gt;&lt;br /&gt;
| orbit_mean_motion     = &amp;lt;!--mean motion of the satellite, usually measured in orbits per day--&amp;gt;&lt;br /&gt;
| orbit_repeat          = &amp;lt;!--repeat interval/revisit time--&amp;gt;&lt;br /&gt;
| orbit_velocity        = &amp;lt;!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity--&amp;gt;&lt;br /&gt;
| orbit_epoch           = &amp;lt;!--the date at which the orbit parameters were correct--&amp;gt;&lt;br /&gt;
| orbit_rev_number      = &amp;lt;!--revolution number--&amp;gt;&lt;br /&gt;
| apsis                 = &amp;lt;!--planet specific apsis term (eg. gee/helion/selene/etc - defaults to generic &amp;quot;apsis&amp;quot;)--&amp;gt;&lt;br /&gt;
|interplanetary         = &amp;lt;!--Infobox spaceflight/IP can be called multiple times for missions with multiple targets or combined orbiter/lander missions, etc--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Cargo parameters--&amp;gt;&lt;br /&gt;
| payload_items         = [[File:India flag-XL-anim.gif|25px]] [[Technology Experiment Satellite|TES]]&amp;lt;br&amp;gt;[[File:Flag of Germany.svg|25px]] [[BIRD (satellite)|BIRD]]&amp;lt;br&amp;gt;[[File:Nuvola Belgian flag.svg|25px]] [[PROBA]]&lt;br /&gt;
| cargo_mass            = {{convert|1294|kg|lbs}}&lt;br /&gt;
| cargo_mass_press      = &amp;lt;!--Mass of pressurised cargo--&amp;gt;&lt;br /&gt;
| cargo_mass_unpress    = &amp;lt;!--Mass of unpressurised cargo (e.g. Dragon Trunk)--&amp;gt;&lt;br /&gt;
| cargo_mass_fuel       = &amp;lt;!--Mass of fuel transferred from spacecraft&amp;#039;s tanks--&amp;gt;&lt;br /&gt;
| cargo_mass_gas        = &amp;lt;!--Mass of gasses transferred (e.g. oxygen)--&amp;gt;&lt;br /&gt;
| cargo_mass_water      = &amp;lt;!--Mass of water transferred--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Telescope parameters--&amp;gt;&lt;br /&gt;
| instrument_type       = &amp;lt;!--converts telescope fields to suit a camera or other similar instrument--&amp;gt;&lt;br /&gt;
| telescope_name        = &amp;lt;!--name, if different to the satellite--&amp;gt;&lt;br /&gt;
| telescope_type        = &amp;lt;!--type of telescope, mirror arrangement, etc--&amp;gt; &lt;br /&gt;
| telescope_diameter    = &amp;lt;!--diameter of telescope--&amp;gt;&lt;br /&gt;
| telescope_focal_length= &amp;lt;!--focal length of telescope--&amp;gt;&lt;br /&gt;
| telescope_area        = &amp;lt;!--collecting area--&amp;gt;&lt;br /&gt;
| telescope_wavelength  = &amp;lt;!--wavelengths at which the telescope operates--&amp;gt; &lt;br /&gt;
| telescope_resolution  = &amp;lt;!--resolution of telescope--&amp;gt;&lt;br /&gt;
| instruments           = &amp;lt;!--a list of instruments on the satellite--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--transponder parameters--&amp;gt;&lt;br /&gt;
| trans_band            = &amp;lt;!--Transponder frequency bands--&amp;gt;&lt;br /&gt;
| trans_frequency       = &amp;lt;!--specific frequencies--&amp;gt;&lt;br /&gt;
| trans_bandwidth       = &amp;lt;!--bandwidth--&amp;gt;&lt;br /&gt;
| trans_capacity        = &amp;lt;!--capacity of the transponders--&amp;gt;&lt;br /&gt;
| trans_coverage        = &amp;lt;!--area covered--&amp;gt;&lt;br /&gt;
| trans_TWTA            = &amp;lt;!--TWTA output power--&amp;gt;&lt;br /&gt;
| trans_EIRP            = &amp;lt;!--equivalent isotropic power--&amp;gt;&lt;br /&gt;
| trans_HPBW            = &amp;lt;!--half-power beam width--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Only use where a spacecraft/mission is part of a clear programme of sequential missions. &lt;br /&gt;
If in doubt, leave it out--&amp;gt;&lt;br /&gt;
| programme             = &amp;#039;&amp;#039;&amp;#039;[[Polar Satellite Launch Vehicle#Launch history|Polar Satellite Launch Vehicle missions]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
| previous_mission      = &amp;#039;&amp;#039;&amp;#039;[[PSLV-C2]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
| next_mission          = &amp;#039;&amp;#039;&amp;#039;[[PSLV-C4]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--mission insignia or patch--&amp;gt;&lt;br /&gt;
| insignia              = &amp;lt;!--omit the &amp;quot;file&amp;quot; prefix--&amp;gt;&lt;br /&gt;
| insignia_caption      = &amp;lt;!--image caption--&amp;gt;&lt;br /&gt;
| insignia_alt          = &amp;lt;!--image alt text--&amp;gt;&lt;br /&gt;
| insignia_size         = &amp;lt;!--include px/em; defaults to 180px--&amp;gt;&lt;br /&gt;
}}&lt;br /&gt;
&amp;#039;&amp;#039;&amp;#039;PSLV-C3&amp;#039;&amp;#039;&amp;#039; was the third operational launch and overall sixth mission of the [[PSLV]] program. This launch was also the forty-sixth launch by [[Indian Space Research Organisation]] since its first mission on 1 January 1962. The vehicle carried three satellites which were deployed in the [[Sun-synchronous orbit|Sun-synchronous]] [[Low Earth orbit]].&amp;lt;ref name=&amp;quot;PSLV-C3&amp;quot;&amp;gt;{{cite news|title=PSLV-C3|publisher=[[Indian Space Research Organisation]]|accessdate=10 Jul 2016|url=http://www.isro.gov.in/launcher/pslv-c3}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 brochure&amp;quot;&amp;gt;{{cite news|title=PSLV-C3 brochure|publisher=[[Indian Space Research Organisation]]|accessdate=10 Jul 2016|url=http://www.isro.gov.in/sites/default/files/pdf/pslv-brochures/PSLVC3.pdf}}&amp;lt;/ref&amp;gt; The vehicle carried [[Technology Experiment Satellite]] (Indian experimental [[earth observation satellite]]), [[BIRD (satellite)|BIRD]] (German [[earth observation satellite]]) and [[PROBA]] (experimental satellite from [[Belgium]]). This was India&amp;#039;s and ISRO&amp;#039;s second commercial [[spaceflight]]. PSLV-C3 was launched at 10:23&amp;amp;nbsp;a.m. [[Indian Standard Time|IST]] on 22 October 2001 from [[Satish Dhawan Space Centre]]  (then called &amp;quot;Sriharikota Range&amp;quot;).&amp;lt;ref name=&amp;quot;PSLV-C3 Successfully Launched : Puts Three Satellites In Orbit&amp;quot;&amp;gt;{{cite news|title=PSLV-C3 Successfully Launched : Puts Three Satellites In Orbit|publisher=defense-aerospace.com|accessdate=10 Jul 2016|url=http://www.defense-aerospace.com/article-view/release/7051/india&amp;#039;s-isro-launches-three-satellites-(oct.-23).html}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;ISRO&amp;#039;s timeline. 1960s to today. #46&amp;quot;&amp;gt;{{cite news|title=ISRO&amp;#039;s timeline. 1960s to today. #46|publisher=[[Indian Space Research Organisation]]|accessdate=10 Jul 2016|url=http://www.isro.gov.in/about-isro/isros-timeline-1960s-to-today#46}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;SPACEWARN Activities&amp;quot;&amp;gt;{{cite news|title=SPACEWARN Activities|publisher=[[NASA]]|accessdate=10 Jul 2016|url=http://nssdc.gsfc.nasa.gov/spacewarn/spx576.html}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;Space Launch Report:  PSLV&amp;quot;&amp;gt;{{cite news|title=Space Launch Report: PSLV|publisher=spacelaunchreport.com|accessdate=10 Jul 2016|url=http://www.spacelaunchreport.com/pslv.html}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 Successfully Launched : Puts 3 Satellites In Orbit&amp;quot;&amp;gt;{{cite news|title=PSLV-C3 Successfully Launched : Puts 3 Satellites In Orbit|publisher=[[Press Information Bureau]]|accessdate=10 Jul 2016|url=http://pib.nic.in/archieve/lreleng/lyr2001/roct2001/22102001/r2210200111.html}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 launches three satellites&amp;quot;&amp;gt;{{cite news|title=PSLV-C3 launches three satellites|publisher=[[The Hindu Business Line]]|accessdate=10 Jul 2016|url=http://www.thehindubusinessline.com/2001/10/23/stories/142367ps.htm}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Mission highlights==&lt;br /&gt;
The mission involved placing Technology Experiment Satellite (TES) and Bispectral and Infrared Remote Detection (BIRD) in a 568&amp;amp;nbsp;km circular orbit. It would then place the PRoject for On Board Autonomy (PROBA) satellite in an 568&amp;amp;nbsp;km x 638&amp;amp;nbsp;km elliptical orbit. This demonstrated ISRO capability to launch multiple satellites in multiple orbits. It also earned ISRO $1 million for each satellite.&amp;lt;ref name=&amp;quot;PSLV-C3&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 brochure&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;:0&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Mission parameters==&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Mass&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;Total liftoff weight:&amp;#039;&amp;#039; {{convert|294000|kg|lbs}}&lt;br /&gt;
** &amp;#039;&amp;#039;Payload weight:&amp;#039;&amp;#039; {{convert|1294|kg|lbs}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Overall height&amp;#039;&amp;#039;&amp;#039;: {{convert|44.4|m|ft|1}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Propellant&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;First stage:&amp;#039;&amp;#039; [[Solid-fuel rocket|Solid]] [[Hydroxyl-terminated polybutadiene|HTPB based]] (138.0 + 54 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; [[Liquid fuel rocket|Liquid]] [[Unsymmetrical dimethylhydrazine|UDMH]] + {{N2O4}} (40 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; [[Solid-fuel rocket|Solid]] [[Hydroxyl-terminated polybutadiene|HTPB based]] (7 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; [[Liquid fuel rocket|Liquid]] [[Monomethylhydrazine|MMH]] + [[Mixed oxides of nitrogen|MON]] (2.0 tonnes)&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Engine&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;First stage:&amp;#039;&amp;#039; S139&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; [[Vikas (rocket engine)|Vikas]]&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; &lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; 2 x PS-4&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;[[Thrust]]&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;First stage:&amp;#039;&amp;#039; 4,430 + 677 x 6 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; 724 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; 324 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; 7.4 x 2 [[Newton (unit)|kN]]&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Altitude&amp;#039;&amp;#039;&amp;#039;: {{convert|586.7|km|mi|0}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Maximum velocity&amp;#039;&amp;#039;&amp;#039;:{{convert|7593|m/s|ft/s|0}} (recorded at time of fourth stage ignition)&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Duration&amp;#039;&amp;#039;&amp;#039;: 1,658 seconds&lt;br /&gt;
&amp;lt;ref name=&amp;quot;PSLV-C3&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 brochure&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV details&amp;quot;&amp;gt;{{cite news|title=PSLV details|publisher=[[Indian Space Research Organisation]]|accessdate=10 Jul 2016|url=http://www.isro.gov.in/launchers/pslv}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Payload==&lt;br /&gt;
PSLV-C3 carried and deployed total three satellites. [[Technology Experiment Satellite]] (TES) was the main payload and BIRD and PROBA were two auxiliary payloads that were mounted on PSLV-C3. In the flight sequence, TES was injected first, followed by BIRD and then PROBA.&amp;lt;ref name=&amp;quot;PSLV-C3&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 brochure&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable sortable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! Country !! Name !! Nos !! Mass !! Type !! Objective&lt;br /&gt;
|-&lt;br /&gt;
| {{Flagicon|India}} India || [[Technology Experiment Satellite|TES]] || 1 || 1,108&amp;amp;nbsp;kg || [[Satellite]]  || Experimental [[Earth observation satellite]]&lt;br /&gt;
|-&lt;br /&gt;
| {{Flagicon|Belgium}} [[Belgium]] || [[BIRD (satellite)|BIRD]] || 1 || 94&amp;amp;nbsp;kg || [[Miniaturized satellite#Microsatellites|Microsatellite]] || [[Remote sensing]] [[technology demonstration]]&lt;br /&gt;
|-&lt;br /&gt;
| {{Flagicon|Germany}} [[Germany]] || [[PROBA]] || 1 || 92&amp;amp;nbsp;kg || [[Miniaturized satellite#Microsatellites|Microsatellite]] || [[Earth observation satellite|Earth observation]] [[technology demonstration]]&lt;br /&gt;
|-&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==Launch &amp;amp; planned flight profile==&lt;br /&gt;
[[File:Full size heat shield of PSLV 7850.JPG|right|thumb|270px|[[Heat shield]] of PSLV displayed at [[Hindustan Aeronautics Limited|HAL]] heritage center.]]&lt;br /&gt;
PSLV-C3 was launched at 10:23&amp;amp;nbsp;a.m. [[Indian Standard Time|IST]] on 22 October 2001 from [[Satish Dhawan Space Centre]]  (then called &amp;quot;Sriharikota Launching Range&amp;quot;). The mission was planned with pre-flight prediction of covering overall distance of {{convert|586.668|km|mi|0}}. The total flight time was 1658 seconds as PROBA was to be launched into an elliptical orbit after TES and BIRD were launched into a circular orbit.&amp;lt;ref name=&amp;quot;:0&amp;quot;&amp;gt;{{Cite web |last=SUBRAMANIAN |first=T. S. |title=An ISRO landmark |url=https://frontline.thehindu.com/science-and-technology/article30252612.ece |access-date=2022-03-25 |website=Frontline |language=en}}&amp;lt;/ref&amp;gt; The orbit raise was done using the yaw RCS thrusters in off-modulated mode.&amp;lt;ref&amp;gt;{{Cite web |title=PSLV-C4 |url=https://www.isro.gov.in/sites/default/files/flipping_book/PSLV-C4/HTML/files/assets/basic-html/page-3.html |access-date=2022-03-26 |website=www.isro.gov.in}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
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Following was the planned flight profile.&amp;lt;ref name=&amp;quot;PSLV-C3&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 brochure&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 Successfully Launched : Puts Three Satellites In Orbit&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;SPACEWARN Activities&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;Space Launch Report: PSLV&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 Successfully Launched : Puts 3 Satellites In Orbit&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C3 launches three satellites&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! [[Multistage rocket|Stage]] !! Time&amp;lt;br&amp;gt;&amp;lt;small&amp;gt;(seconds)&amp;lt;/small&amp;gt;!! Altitude &amp;lt;br&amp;gt;&amp;lt;small&amp;gt;(kilometer)&amp;lt;/small&amp;gt; !! Velocity&amp;lt;br&amp;gt;&amp;lt;small&amp;gt;(meter/sec)&amp;lt;/small&amp;gt; !! Event !! Remarks&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;6&amp;quot; | [[Multistage rocket|First stage]] || T+0 || rowspan=&amp;quot;2&amp;quot; | 0.02 || rowspan=&amp;quot;2&amp;quot; | 452 || First stage ignition || Lift-off&lt;br /&gt;
|-&lt;br /&gt;
| T+1.24 || Ignition of 4 ground-lit strap-on motors || &lt;br /&gt;
|-&lt;br /&gt;
| T+25.04 || 2.515 || 551 || Ignition of 2 air-lit strap-on motors || &lt;br /&gt;
|-&lt;br /&gt;
| T+68.04 || 23.472 || 1,155 || Separation of 4 ground-lit strap-on motors || &lt;br /&gt;
|-&lt;br /&gt;
| T+90.04 || 40.061 || 1,644 || Separation of 2 air-lit strap-on motors || &lt;br /&gt;
|-&lt;br /&gt;
| T+112.73 || 67.601 || 2,028 || First stage separation || &lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;3&amp;quot; | [[Multistage rocket|Second stage]] || T+112.93 || 67.828 || 2,027 || Second stage ignition || &lt;br /&gt;
|-&lt;br /&gt;
| T+156.73 || 115.604 || 2,284 || [[Heat shield]] separation ||&lt;br /&gt;
|-&lt;br /&gt;
| T+278.81 || 236.272 || 4,099 || Second stage separation ||&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; | [[Multistage rocket|Third stage]] || T+280.01 || 237.433 || 4,097 || Third stage ignition || &lt;br /&gt;
|-&lt;br /&gt;
| T+498.33 || 455.487 || 6,086 || Third stage separation || &lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;7&amp;quot; | [[Multistage rocket|Fourth stage]] || T+520.60 || 460.818 || 6,065 || Fourth stage ignition || &lt;br /&gt;
|-&lt;br /&gt;
| T+914.92 || 571.247 || rowspan=&amp;quot;4&amp;quot; | 7,575 || Fourth stage thrust cut-off ||&lt;br /&gt;
|-&lt;br /&gt;
| T+971.92 || 572.080 || [[Technology Experiment Satellite|TES]] separation ||&lt;br /&gt;
|-&lt;br /&gt;
| T+1,011.92 || 572.709 || [[BIRD (satellite)|BIRD]] separation ||&lt;br /&gt;
|-&lt;br /&gt;
| T+1,091.92 || 574.064 || [[PROBA]] orbit raise start ||&lt;br /&gt;
|-&lt;br /&gt;
| T+1,552.50 || 585.018 || 7,593 || PROBA orbit raise stop ||&lt;br /&gt;
|-&lt;br /&gt;
| T+1,602.50 || 586.688 || 7,592 || PROBA orbit separation || Mission over&lt;br /&gt;
|-&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==Fourth Stage Break-up event==&lt;br /&gt;
The fourth stage of the PSLV had undergone a break-up event on 19 December 2001, likely caused by an explosion.&amp;lt;ref&amp;gt;{{cite conference |last1=Bandyopadhyay |first1=Parthasarathi |last2=Sharma |first2=Radhey |last3=Adimurthy |first3=V. |title=Analysis of the possible cause of break up of PSLV-C3/PS4 stage |url=https://ui.adsabs.harvard.edu/abs/2002cosp...34E1374B/abstract |conference=34th COSPAR Scientific Assembly |publisher=The Second World Space Congress |place=Houston, Texas |date=October 2002 |page=1374 |bibcode=2002cosp...34E1374B }}&amp;lt;/ref&amp;gt; After the explosion of PSLV-C3, ISRO carried out passivation of the upper stages of the PSLV, from the PSLV-C4 mission onwards.&amp;lt;ref&amp;gt;{{Cite journal |last=Kosambe |first=Santosh |date=2019 |title=Overview of the Space Debris Mitigation Activities in ISRO |url=https://www.researchgate.net/publication/336366346 |journal=Journal of Aircraft and Space Technology |volume=3 |pages=199–200 |via=ResearchGate}}&amp;lt;/ref&amp;gt; As per ISRO, this event generated 386 debris objects, of which 76 are still in orbit, as on 2021.&amp;lt;ref&amp;gt;{{Cite web |author=Chethan Kumar|date=Mar 25, 2022 |title=In 2021, 135 launches put 1.8k objects in space, 102 launches put 522 objects in 2020; Isro flags off debris concern {{!}} India News - Times of India |url=https://timesofindia.indiatimes.com/india/in-2021-135-launches-put-1-8k-objects-in-space-102-launches-put-522-objects-in-2020-isro-flags-off-debris-concern/articleshow/90448200.cms |access-date=2022-03-26 |website=The Times of India |language=en}}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{Cite web |title=Space Situational Assessment 2021 - ISRO |url=https://www.isro.gov.in/update/24-mar-2022/space-situational-assessment-2021 |access-date=2022-03-26 |website=www.isro.gov.in}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
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{{Portal bar|India|Science|Space|Spaceflight}}&lt;br /&gt;
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==See also==&lt;br /&gt;
* [[Indian Space Research Organisation]]&lt;br /&gt;
* [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
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== References ==&lt;br /&gt;
{{Reflist|colwidth=30em}}&lt;br /&gt;
{{PSLV}}&lt;br /&gt;
{{Indian space programme}}&lt;br /&gt;
{{Expendable launch systems}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Spacecraft launched in 2001]]&lt;br /&gt;
[[Category:Polar Satellite Launch Vehicle]]&lt;/div&gt;</summary>
		<author><name>Ajay Kumar</name></author>
	</entry>
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