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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 electrical capacity consignment to LEO 3,250 kilograms (7,200 lb) Payload to SSO 1,600 kilograms (3,500 lb) open 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) arise line deliver Engines1 solid Thrust4,860 kN Specific impulse 269sec cut off time one hundred five seconds FuelHTPB (solid) Second peak Engines1 Vikas Thrust725 kN Specific impulse 293 sec issue time158 seconds FuelN2O4/UDMH Third deliver Engines1 solid Thrust328 kN Specific impulse 294 sec Burn time83 seconds FuelSolid one-fourth face Engines2 unstable Thrust14 kN Specific impulse 308 sec Burn time425 seconds FuelMMH/UDMH The PSLV has four stages using solid and liquid propulsion systems alternately.

The exit-go stage is one of the largest solid- burn rocket boosters in the reality 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 force out and Nitrogen tetroxide (N2O4) as oxidizer. The third stage uses 7 t onnes of HTPB-based solid propellant and pro! duces a maximum thrust of 324 kN.. For run engage 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 get a full essay, order it on our website: BestEssayCheap.com

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