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	<title>PSLV-C6 - Revision history</title>
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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-C6&lt;br /&gt;
| names_list            = HAMSAT mission&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--image of the spacecraft/mission--&amp;gt;&lt;br /&gt;
| image                 = The PSLV – C6 on its mobile pedestal after having been strapped to launch tower at Sriharikota on May 1, 2005 (1).jpg&lt;br /&gt;
| image_caption         = The PSLV – C6 on its mobile pedestal after having been strapped to launch tower at Sriharikota on 1 May 2005&lt;br /&gt;
| image_alt             = &amp;lt;!--image alt text--&amp;gt;&lt;br /&gt;
| image_size            =&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Basic details--&amp;gt;&lt;br /&gt;
| mission_type          = Deployment of two [[satellite]]s.&lt;br /&gt;
| operator              =[[ISRO]]&lt;br /&gt;
| Harvard_designation   = &amp;lt;!--spacecraft launched 1962 and earlier only (e.g. 1957 Alpha 2)--&amp;gt;&lt;br /&gt;
| COSPAR_ID             = &amp;lt;!--spacecraft launched since 1963 only (aka NSSDC ID; e.g. 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      = 1,120 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     =&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;!--e.g. A2100M, Star-2, etc--&amp;gt;&lt;br /&gt;
| manufacturer          =[[ISRO]]&lt;br /&gt;
| launch_mass           = {{convert|295980|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|1,602.5|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|2005|05|05|04|44|00|7=UTC}} ([[Coordinated Universal Time|UTC]])&lt;br /&gt;
| launch_rocket         = [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
| launch_site           = [[Satish Dhawan Space Centre Second Launch Pad|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|2005|05|05}}&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]]&lt;br /&gt;
| orbit_regime          = &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;!--orbit 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 (e.g. 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]] [[Cartosat-1]]&amp;lt;br&amp;gt;[[File:India flag-XL-anim.gif|25px]] [[HAMSAT]]&lt;br /&gt;
| cargo_mass            = {{convert|1,602.5|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-C5]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
| next_mission          = &amp;#039;&amp;#039;&amp;#039;[[PSLV-C7]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--mission insignia or patch--&amp;gt;&lt;br /&gt;
| insignia              =&lt;br /&gt;
| insignia_caption      = PSLV-C6, [[HAMSAT]] &amp;amp; [[IRS-P5]] combined insignia&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;
&lt;br /&gt;
&amp;#039;&amp;#039;&amp;#039;PSLV-C6&amp;#039;&amp;#039;&amp;#039; was the sixth operational launch and overall ninth mission of the [[PSLV]] program. This launch was also the fifty-fourth launch by [[Indian Space Research Organisation]] since its first mission on 1 January 1962. The vehicle carried and injected India&amp;#039;s two [[satellite]]s; [[Cartosat-1]] (a.k.a. IRS-P5) and [[HAMSAT]] into the [[Sun-synchronous orbit]]. PSLV-C6 was launched at 04:44 hours [[Coordinated Universal Time]] (10:14 hours [[Indian Standard Time]]) on 5 May 2005 from the [[Satish Dhawan Space Centre Second Launch Pad|second launch pad]] of the [[Satish Dhawan Space Centre]].&amp;lt;ref name=&amp;quot;PSLV series&amp;quot;&amp;gt;{{cite news|title=PSLV series|publisher=astronautix.com|accessdate=28 August 2016|url=http://www.astronautix.com/p/pslv.html|archive-url=https://web.archive.org/web/20160820033519/http://astronautix.com/p/pslv.html|url-status=dead|archive-date=August 20, 2016}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C6: A path-breaking launch&amp;quot;&amp;gt;{{cite news|title=PSLV-C6: A path-breaking launch|publisher=[[Business Standard]]|accessdate=28 August 2016|url=http://www.business-standard.com/article/opinion/devangshu-datta-pslv-c6-a-path-breaking-launch-105051201010_1.html}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;ISRO scientists meet Prime Minister&amp;quot;&amp;gt;{{cite news|title=ISRO scientists meet Prime Minister|publisher=[[Indian Space Research Organisation]]|accessdate=28 August 2016|url=http://www.isro.gov.in/category-launchers/pslv-c6}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;India&amp;#039;s PSLV-C6 Successfully Launches 2 Satellites&amp;quot;&amp;gt;{{cite news|title=India&amp;#039;s PSLV-C6 Successfully Launches 2 Satellites|publisher=spaceref.com|accessdate=28 August 2016|url=http://www.spaceref.com/news/viewpr.html?pid=16830}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C6 launched from Sriharikota&amp;quot;&amp;gt;{{cite news|title=PSLV-C6 launched from Sriharikota|publisher=[[The Economic Times]]|accessdate=28 August 2016|url=http://articles.economictimes.indiatimes.com/2005-05-05/news/27496736_1_hamsat-launch-pad-cartosat-1}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Mission highlights==&lt;br /&gt;
*Sixth operational launch of the [[PSLV]] program.&lt;br /&gt;
*Overall ninth mission of the [[PSLV]] program.&lt;br /&gt;
*Overall fifty-fourth launch by [[Indian Space Research Organisation]].&lt;br /&gt;
*First flight to be launched from the [[Satish Dhawan Space Centre Second Launch Pad|second launch pad]] of [[Satish Dhawan Space Centre]].&lt;br /&gt;
*Carried and injected two satellites built by [[Indian Space Research Organisation|ISRO]].&amp;lt;ref name=&amp;quot;PSLV-C6&amp;quot;&amp;gt;{{cite news|title=PSLV-C6|publisher=[[Indian Space Research Organisation]]|accessdate=28 August 2016|url=http://www.isro.gov.in/launcher/pslv-c6}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;PSLV&amp;quot;&amp;gt;{{cite news|title=PSLV|publisher=spacelaunchreport.com|accessdate=28 August 2016|url=http://www.spacelaunchreport.com/pslv.html}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;ISRO timeline&amp;quot;&amp;gt;{{cite news|title=ISRO timeline|publisher=[[Indian Space Research Organisation]]|accessdate=28 August 2016|url=http://www.isro.gov.in/about-isro/isros-timeline-1960s-to-today#54}}&amp;lt;/ref&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|295980|kg|lbs}}&lt;br /&gt;
** &amp;#039;&amp;#039;Payload weight:&amp;#039;&amp;#039; {{convert|1,602.5|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 + 6 x 9 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; [[Liquid fuel rocket|Liquid]] [[UH 25]] + {{N2O4}} (41.5 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; [[Solid-fuel rocket|Solid]] [[Hydroxyl-terminated polybutadiene|HTPB based]] (7.6 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]] (2.5 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; Core (PS 1) + 6 strap-on [[Propellant strap on motor|PSOM]]&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; PS 3&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; 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; 4,762 + 645 x 6 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; 800 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; 246 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; 7.3 x 2 [[Newton (unit)|kN]]&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Altitude&amp;#039;&amp;#039;&amp;#039;: {{convert|628.535|km|mi|0}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Maximum velocity&amp;#039;&amp;#039;&amp;#039;:{{convert|7546|m/s|ft/s|0}} (recorded at time of payload separation)&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Duration&amp;#039;&amp;#039;&amp;#039;: 1,120 seconds&lt;br /&gt;
&amp;lt;ref name=&amp;quot;PSLV-C6&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C6 brochure&amp;quot;&amp;gt;{{cite news|title=PSLV-C6 brochure|publisher=[[Indian Space Research Organisation]]|accessdate=28 August 2016|url=http://www.isro.gov.in/sites/default/files/pdf/pslv-brochures/PSLVC6.pdf}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Payload==&lt;br /&gt;
PSLV-C6 carried and deployed two Indian satellites, [[Cartosat-1]] (a.k.a. IRS-P5) and [[HAMSAT]] into the [[Sun-synchronous orbit]]. Built by [[Indian Space Research Organisation|ISRO]], Cartosat-1 was a stereoscopic [[remote sensing satellite]] and first of the [[Cartosat]] series of satellites.&amp;lt;ref name=&amp;quot;PSLV-C6 launched from Sriharikota&amp;quot;/&amp;gt; HAMSAT was a [[Miniaturized satellite#Microsatellites|microsatellite]], built for providing satellite based [[amateur radio satellite]] to the national as well as the international community of [[amateur radio operator]]s (HAM).&amp;lt;ref name=&amp;quot;HAMSAT&amp;quot;&amp;gt;{{cite news|title=HAMSAT|publisher=[[Indian Space Research Organisation]]|accessdate=28 August 2016|url=http://www.isro.gov.in/category-spacecraft/hamsat}}&amp;lt;/ref&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;
| rowspan=&amp;quot;2&amp;quot; | {{Flagicon|India}} India || [[IRS-P5]] || 1 || 1,560&amp;amp;nbsp;kg || [[Satellite]] || [[Remote sensing satellite]]&lt;br /&gt;
|-&lt;br /&gt;
| [[HAMSAT]] || 1 || 42.5&amp;amp;nbsp;kg || [[Miniaturized satellite#Microsatellites|Microsatellite]] || [[Amateur radio satellite]]&lt;br /&gt;
|-&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==Launch &amp;amp; planned flight profile==&lt;br /&gt;
[[File:PS LV-C 6 blasting off from launch Tower at Sriharikota on May 5, 2005.jpg|thumb|PSLV-C 6 blasting off from launch Tower at Sriharikota on May 5, 2005]]&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-C6 was launched at 04:44 hours [[Coordinated Universal Time]] (10:14 hours [[Indian Standard Time]]) on 5 May 2005 from the [[Satish Dhawan Space Centre Second Launch Pad|second launch pad]] of the [[Satish Dhawan Space Centre]]. The mission was planned with pre-flight prediction of covering overall distance of {{convert|622|km|mi|0}}. Following was the flight profile.&amp;lt;ref name=&amp;quot;PSLV-C6 brochure&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 || 0.025 || 452 || Ignition of PS 1 || Lift off&lt;br /&gt;
|-&lt;br /&gt;
| T+1.19 || 0.026 || 452 || Ignition of 4 ground-lit [[Propellant strap on motor|PSOM]] ||&lt;br /&gt;
|-&lt;br /&gt;
| T+25 || 2.463 || 551 || Ignition of 2 air-lit PSOM ||&lt;br /&gt;
|-&lt;br /&gt;
| T+68 || 23.748 || 1,179 || Separation of 4 ground-lit PSOM ||&lt;br /&gt;
|-&lt;br /&gt;
| T+90 || 42.768 || 1,659 || Separation of 2 air-lit PSOM ||&lt;br /&gt;
|-&lt;br /&gt;
| T+112.03 || 67.411 || 1,995 || Separation of PS 1 ||&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;3&amp;quot; | [[Multistage rocket|Second stage]] || T+112.23 || 67.635 || 1,994 || Ignition of PS 2 ||&lt;br /&gt;
|-&lt;br /&gt;
| T+156.03 || 115.244 || 2,314 || Separation of [[heat shield]] ||&lt;br /&gt;
|-&lt;br /&gt;
| T+263.38 || 233.873 || 4,087 || Separation of PS 2 ||&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; | [[Multistage rocket|Third stage]] || T+264.58 || 235.304 || 4,083 || Ignition of HPS 3 ||&lt;br /&gt;
|-&lt;br /&gt;
| T+517.52 || 498.974 || 5,865 || Separation of HPS 3 ||&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;4&amp;quot; | [[Multistage rocket|Fourth stage]] || T+531.50 || 509.092 || 5,851 || Ignition of PS 4 ||&lt;br /&gt;
|-&lt;br /&gt;
| T+1,043.62 || 627.153 || 7,542 || Cut-off of PS 4 ||&lt;br /&gt;
|-&lt;br /&gt;
| T+1,080.62 || 627.801 || 7,546 || [[Cartosat-1]] separation || &lt;br /&gt;
|-&lt;br /&gt;
| T+1,120.62 || 628.535 || 7,546 || [[HAMSAT]] separation || Mission complete&lt;br /&gt;
|-&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
* [[Indian Space Research Organisation]]&lt;br /&gt;
* [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
&lt;br /&gt;
{{Portal bar|India|Science|Space|Spaceflight}}&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
{{Reflist|colwidth=30em}}&lt;br /&gt;
&lt;br /&gt;
== External links ==&lt;br /&gt;
{{Commons category-inline|PSLV-C6}}&lt;br /&gt;
&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 2005]]&lt;br /&gt;
[[Category:Polar Satellite Launch Vehicle]]&lt;/div&gt;</summary>
		<author><name>Ajay Kumar</name></author>
	</entry>
</feed>