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PSLV C-11 FunctionExpendable launch vehicle ManufacturerISRO Country of downslope 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) set up history StatusActive Launch sitesSriharikota Total launches14 Successes12 Failures1 partial t champion failures1 maiden over flight20 folk 1993 Boosters (Stage 0) No boosters6 Engines1 unattackable fox502.600 kN specialized impulse 262 sec swinge time44 seconds raiseHTPB ( material) scratch line acquaint Engines1 solid Thrust4,860 kN limited impulse 269sec Burn time one hundred five seconds FuelHTPB (solid) due south stage Engines1 Vikas Thrust725 kN Specific impulse 293 sec Burn time158 seconds FuelN2O4/UDMH 3rd stage Engines1 solid Thrust328 kN Specific impulse 294 sec Burn time83 seconds FuelSolid tail stage Engines2 mobile Thrust14 kN Specific impulse 308 sec Burn time425 seconds FuelMMH/UDMH The PSLV has quaternion stages using solid and liquid propulsion systems alternately.

The setoff stage is one of the largest solid- burn rise boosters in the world and carries 138 tonnes of Hydroxyl-terminated polybutadiene (HTPB) springtime propellent with a diameter 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 fire and Nitrogen tetroxide (N2O4) as oxidizer. The third stage uses 7 tonnes of HTPB-based solid propellant and produces a uttermost thrust of 324 kN.. For roll lease it uses the RCS (Reaction Control System) of fourth stage. The fourth and the terminal stage of PSLV has a twin engine form 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 commencement mission...If you want to get a full essay, order it on our website: Ordercustompaper.com

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