PSLV-C1
{{Use British English|date=October 2021}}
{{Use dmy dates|date=October 2021}}
{{Infobox spaceflight
| name = PSLV-C1
| image = PSLV.svg
| image_caption = Model of the PSLV rocket
| image_size = 70px
| mission_type = Deployment of one satellite
| operator = ISRO
| COSPAR_ID =
| SATCAT =
| website = [http://www.isro.gov.in/ ISRO website]
| mission_duration = 1090.52 seconds
| spacecraft = Polar Satellite Launch Vehicle
| spacecraft_type = Launch vehicle
| spacecraft_bus =
| manufacturer = ISRO
| launch_mass = {{cvt|294000|kg}}
| payload_mass = {{cvt|1250|kg}}
| dimensions =
| power =
| launch_date = 29 September 1997, 04:47 UTC
| launch_rocket = PSLV
| launch_site = Sriharikota Launching Range
| launch_contractor = ISRO
| orbit_reference = Geocentric orbit
| orbit_regime = Sun-synchronous orbit
| orbit_periapsis =
| orbit_apoapsis =
| orbit_inclination = 98.7°
| apsis = gee
| payload_items = IRS-1D
| insignia =
| insignia_caption =
| insignia_size = 200px
| programme = Polar Satellite Launch Vehicle missions
| previous_mission = PSLV-D3
| next_mission = PSLV-C2
}}
PSLV-C1 was the overall fourth mission of the Polar Satellite Launch Vehicle (PSLV) program by Indian Space Research Organisation (ISRO). The vehicle carried IRS-1D satellite which was deployed in the Sun-synchronous orbit (SSO).{{cite news|title=PSLV-C1|publisher=Indian Space Research Organisation|access-date=24 Jun 2016|url=http://www.isro.gov.in/launcher/pslv-c1}}{{cite news|title=PSLV-C1 brochure|publisher=Indian Space Research Organisation|access-date=24 June 2016|url=http://www.isro.gov.in/sites/default/files/pdf/pslv-brochures/PSLVC1.pdf}}{{cite news|url=http://www.spacelaunchreport.com/pslv.html|archive-url=https://archive.today/20130104225437/http://www.spacelaunchreport.com/pslv.html|url-status=usurped|archive-date=4 January 2013|title=PSLV|publisher=Space Launch Report|access-date=24 June 2016}}{{cite news|title=ISRO Timeline|publisher=Indian Space Research Organisation|access-date=24 June 2016|url=http://www.isro.gov.in/about-isro/isros-timeline-1960s-to-today#39}} This was India's first launch vehicle built without Russian assistance and PSLV's first operational flight placed IRS-1D into a polar orbit. However, it could not place the satellite in the desired circular orbit but in an elliptical orbit due to a leak of helium gas from one of the components. The mission was termed partial failure since the satellite could not be placed at the desired altitude.{{cite news |title=Space|publisher=digitaltoday.in|access-date=24 June 2016|url=http://archives.digitaltoday.in/indiatoday/13101997/space.html}}{{cite news|title=PSLV fail |publisher=spacelaunchreport.com|access-date=24 June 2016|url=http://www.spacelaunchreport.com/slvfail.txt|archive-url=https://archive.today/20120913053550/http://www.spacelaunchreport.com/slvfail.txt|url-status=usurped|archive-date=13 September 2012}}
Mission parameters
- Mass:
- Total liftoff weight: {{cvt|294000|kg}}
- Payload weight: {{cvt|1250|kg}}
- Overall height: {{cvt|44.4|m}}
- Propellant:
- Stage 1: Solid HTPB based
- Stage 2: Liquid UH 25 + {{N2O4}}
- Stage 3: Solid HTPB based
- Stage 4: Liquid MMH + MON-3
- Altitude: {{cvt|826|km}}
- Maximum velocity: {{cvt|7436|m/s}} (recorded at time of fourth stage cut-off)
- Inclination: 98.7°
Launch
PSLV-C1 was launched at 04:47 UTC on 29 September 1997 from Satish Dhawan Space Centre (then called "Sriharikota Launching Range"). The vehicle placed the IRS-1D satellite in the Sun-synchronous orbit.
See also
References
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{{Portal bar|India|Science|Space|Spaceflight}}
{{PSLV}}
{{Indian space programme}}
{{Expendable launch systems}}