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PSLV C-11 FunctionExpendable launch vehicle ManufacturerISRO Country of blood India Size Height44 metres (140 ft) Diameter2.8 metres (9.2 ft) Mass294,000 kilograms (650,000 lb) Stages4 Capacity consignment to LEO 3,250 kilograms (7,200 lb) Payload to SSO 1,600 kilograms (3,500 lb) frame history StatusActive Launch sitesSriharikota Total launches14 Successes12 Failures1 partial failures1 maiden over flight20 kinfolk 1993 Boosters (Stage 0) No boosters6 Engines1 unattackable fox502.600 kN specialized impulse 262 sec blaze time44 seconds raiseHTPB ( substantialness) scratch line coiffure Engines1 solid Thrust4,860 kN special impulse 269sec Burn time superstar hundred five seconds FuelHTPB (solid) encourage stage Engines1 Vikas Thrust725 kN Specific impulse 293 sec Burn time158 seconds FuelN2O4/UDMH ordinal stage Engines1 solid Thrust328 kN Specific impulse 294 sec Burn time83 seconds FuelSolid quaternary stage Engines2 lucid Thrust14 kN Specific impulse 308 sec Burn time425 seconds FuelMMH/UDMH The PSLV has quartette stages using solid and liquid propulsion systems alternately.

The setoff stage is one of the largest solid- burn rocket locomotive boosters in the world and carries 138 tonnes of Hydroxyl-terminated polybutadiene (HTPB) natural spring propelling with a diam of 2.8 m. The second stage employs the Vikas engine and carries 41.5 tonnes (40 tonnes till C-5 mission) of liquid propellant Unsymmetrical Di-Methyl Hydrazine (UDMH) as force out and Nitrogen tetroxide (N2O4) as oxidizer. The thirdly stage uses 7 tonnes of HTPB-based solid propellant and produces a utmost thrust of 324 kN.. For roll rent it uses the RCS (Reaction Control System) of stern stage. The fourth and the terminal stage of PSLV has a twin engine descriptor using liquid propellant. With a propellant loading of 2 tonnes (Mono-Methyl Hydrazine as fuel + liquefy Oxides of Nitrogen as oxidiser. Chandrayaan-1,Moon-vehicle is Indias maiden mission...If you want to get a full essay, order it on our website: Orderessay

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