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PSLV-C1

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]

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 →
 

Mission parameters Edit

  • Mass:
    • Total liftoff weight: 294,000 kg (648,000 lb)
    • Payload weight: 1,250 kg (2,760 lb)
  • Overall height: 44.4 m (146 ft)
  • Propellant:
    • Stage 1: Solid HTPB based
    • Stage 2: Liquid UH 25 + N2O4
    • Stage 3: Solid HTPB based
    • Stage 4: Liquid MMH + MON-3
  • Altitude: 826 km (513 mi)
  • Maximum velocity: 7,436 m/s (24,400 ft/s) (recorded at time of fourth stage cut-off)
  • Inclination: 98.7°
  • Period: 1090.52 seconds [2]

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.
  2. ^ a b c "PSLV-C1 brochure" (PDF). Indian Space Research Organisation. Retrieved 24 June 2016.
  3. ^ a b "PSLV". Space Launch Report. Retrieved 24 June 2016.
  4. ^ a b "ISRO Timeline". Indian Space Research Organisation. Retrieved 24 June 2016.
  5. ^ a b "Space". digitaltoday.in. Retrieved 24 June 2016.
  6. ^ "PSLV fail". spacelaunchreport.com. Retrieved 24 June 2016.

pslv, overall, fourth, mission, polar, satellite, launch, vehicle, pslv, program, indian, space, research, organisation, isro, vehicle, carried, satellite, which, deployed, synchronous, orbit, this, india, first, launch, vehicle, built, without, russian, assis. 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 PSLV C1Model of the PSLV rocketMission typeDeployment of one satelliteOperatorISROWebsiteISRO websiteMission duration1090 52 secondsSpacecraft propertiesSpacecraftPolar Satellite Launch VehicleSpacecraft typeLaunch vehicleManufacturerISROLaunch mass294 000 kg 648 000 lb Payload mass1 250 kg 2 760 lb Start of missionLaunch date29 September 1997 04 47 UTCRocketPSLVLaunch siteSriharikota Launching RangeContractorISROOrbital parametersReference systemGeocentric orbitRegimeSun synchronous orbitInclination98 7 PayloadIRS 1DPolar Satellite Launch Vehicle missions PSLV D3PSLV C2 Contents 1 Mission parameters 2 Launch 3 See also 4 ReferencesMission parameters EditMass Total liftoff weight 294 000 kg 648 000 lb Payload weight 1 250 kg 2 760 lb Overall height 44 4 m 146 ft Propellant Stage 1 Solid HTPB based Stage 2 Liquid UH 25 N2O4 Stage 3 Solid HTPB based Stage 4 Liquid MMH MON 3Altitude 826 km 513 mi Maximum velocity 7 436 m s 24 400 ft s recorded at time of fourth stage cut off Inclination 98 7 Period 1090 52 seconds 2 Launch EditPSLV 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 EditIndian Space Research Organisation Polar Satellite Launch VehicleReferences Edit 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 Retrieved 24 June 2016 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 Retrieved 24 June 2016 Portals India Science Space Spaceflight Retrieved from https en wikipedia org w index php title PSLV C1 amp oldid 1051165725, wikipedia, wiki, book, books, library,

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