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PSLV C-11 FunctionExpendable launch vehicle ManufacturerISRO Country of declivity India Size Height44 metres (140 ft) Diameter2.8 metres (9.2 ft) Mass294,000 kilograms (650,000 lb) Stages4 talent consignment to LEO 3,250 kilograms (7,200 lb) Payload to SSO 1,600 kilograms (3,500 lb) absorb history StatusActive Launch sitesSriharikota Total launches14 Successes12 Failures1 Partial failures1 maiden over flight20 September 1993 Boosters (Stage 0) No boosters6 Engines1 unattackable fox502.600 kN specialized impulse 262 sec singe time44 seconds raiseHTPB (solid) cicatrix line acquaint Engines1 solid Thrust4,860 kN Specific impulse 269sec singe time one hundred five seconds FuelHTPB (solid) Second represent Engines1 Vikas Thrust725 kN Specific impulse 293 sec write out time158 seconds FuelN2O4/UDMH Third peak Engines1 solid Thrust328 kN Specific impulse 294 sec Burn time83 seconds FuelSolid fourthly floor Engines2 liquifiable Thrust14 kN Specific impulse 308 sec Burn time425 seconds FuelMMH/UDMH The PSLV has four stages using solid and liquid propulsion systems alternately.

The kickoff stage is one of the largest solid- burn rocket boosters in the homo and carries 138 tonnes of Hydroxyl-terminated polybutadiene (HTPB) outflow propellant 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 send away and Nitrogen tetroxide (N2O4) as oxidizer. The third stage uses 7 tonnes of HTPB-based solid propellant and produces a max imum thrust of 324 kN.. For divagate engag! e it uses the RCS (Reaction Control System) of fourth stage. The fourth and the terminal stage of PSLV has a twin engine configuration using liquid propellant. With a propellant loading of 2 tonnes (Mono-Methyl Hydrazine as fuel + commingle Oxides of Nitrogen as oxidiser. Chandrayaan-1,Moon-vehicle is Indias first mission...If you want to shrink a full essay, order it on our website: OrderEssay.net

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