Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Mission parameters  





2 Launch  





3 See also  





4 References  














PSLV-C1







ி
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


PSLV-C1
Model of the PSLV rocket
Mission typeDeployment of one satellite
OperatorISRO
WebsiteISRO website
Mission duration1090.52 seconds
Spacecraft properties
SpacecraftPolar Satellite Launch Vehicle
Spacecraft typeLaunch vehicle
ManufacturerISRO
Launch mass294,000 kg (648,000 lb)
Payload mass1,250 kg (2,760 lb)
Start of mission
Launch date29 September 1997, 04:47 UTC
RocketPSLV
Launch siteSriharikota Launching Range
ContractorISRO
Orbital parameters
Reference systemGeocentric orbit
RegimeSun-synchronous orbit
Inclination98.7°
Payload
IRS-1D
← PSLV-D3
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).[1][2][3][4] 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.[5][6]

Mission parameters[edit]

Launch[edit]

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.[1][2][3][4][5]

See also[edit]

References[edit]

  1. ^ a b "PSLV-C1". Indian Space Research Organisation. Retrieved 24 June 2016.
  • ^ a b c "PSLV-C1 brochure" (PDF). Indian Space Research Organisation. Retrieved 24 June 2016.
  • ^ a b "PSLV". Space Launch Report. Archived from the original on 4 January 2013. Retrieved 24 June 2016.{{cite news}}: CS1 maint: unfit URL (link)
  • ^ a b "ISRO Timeline". Indian Space Research Organisation. Retrieved 24 June 2016.
  • ^ a b "Space". digitaltoday.in. Retrieved 24 June 2016.
  • ^ "PSLV fail". spacelaunchreport.com. Archived from the original on 13 September 2012. Retrieved 24 June 2016.{{cite news}}: CS1 maint: unfit URL (link)
  • icon Science
  • Space
  • Spaceflight

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=PSLV-C1&oldid=1197845703"

    Categories: 
    Spacecraft launched in 1997
    Polar Satellite Launch Vehicle
    Hidden categories: 
    CS1 maint: unfit URL
    Use British English from October 2021
    Use dmy dates from October 2021
     



    This page was last edited on 22 January 2024, at 04:13 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki