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WITH THE TOUCH OF GEOSYNCHOROUS SATELLITE LAUNCH VEHICLE (GSLVD-1) FROM ITS LAUNCH PAD ON THE SRI HARIKOTA ISLAND SHORTLY AS ON MARCH 6,001,IT IS LANDMARK OF THE INDIAN SPACE RESERCH ORGANISATION.THE MISSIONS SUCCESS WILL MEAN INDIA WILL BE ABLE ON ITS OWN TO PLACE IN ORBIT ITS COMMUNICATION SATELLITES.ALL THE INSAT SERIES SATELLITES WERE LAUNCED FROM ABROAD-KOUROU,FRANCE,ENGLAN AND UNITED STATES
THE 4 TONNES,44 METER TALL PSLV INJECTED A 1050KG INDIAN REMOTE SENSING SATELLITE INTO A POLOR ORBIT AT AN ALTITUDE OF 80KM ABOVE THE EARTH .THE GSLV,44-METERS TALL AND WEIGHTS 401 TONNES,SATELLITE WITH A 7 METER,00 TONNE MULTIPLATFORM MOBILE SERVICES POWER.
IT WILL PALCES THE 1,540 KG EXPERIMENTAL COMMUNICATION GEOSYNCHOROROUS SATELLITE IN AN ELLPTICAL GEOSYNCHRONOUS TRANSFER ORBIT.THE ELLISPE WILL HAVE A PERIGEE 0F 185 KM AND AN APOGEES OF 6,000KM.THE SATELLITE IS PROPULSION SYSTEMS WILL BE FIRED TO ATTAIN A CIRCULAR ORBIT OF 6,000 KM RADIUS.
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THE FIRST STAGE OF THE GSLV COMPRISES A SOLID PREPELLANTMOTOR.THE CORE IS POWERED BY 1TONNES OF SOLID PROPELLANTS AND THERE ARE FOUR LIQUID STRAP ON MOTORS STRUNG AROUND THE CORE.THE LIQUID PROPELLANTS IN EACH OF THE STRAP ON MOTORS WEIGH 40TONNES.THE SECOND STAGE HAS 1.5 TONNES OF LIQUID PROPELLANTS.THE THIRD IS AYOGENIC STAGE THAT USES 1.5TONNES OF LIQUID HYDROGEN AND LIQUID OXYGEN.THE LIQUID STRAP ON MOTORS ARE FIRST IGNITED AND THE CORE SOLID IS FIRED AFTER A GAP OF 4.6TONNES.
GSLV IS A MUCH MORE COMPLEN VEHICLE THAN THE GSLV.IT USES FIVE LIQUID MOTORS WHILE THE PSLV HAD SIX SOLID STRAP OF MOTORS.
ANOTHER DIFFERENT IS THE MANNER OF FIRING OFTHE STRAPONS.DR.KASTURIIRONGON,WHO SAID THAT HE WAS VERY CONFIDENT OF THE SUCCESS,NEVERTHLESS SPOKE ABOUT THE GAPS WHILE EMPHOSSING THE DEVELOPEMENT NATURE OF THE LIGHT.
THE GAPS IN THE VEHICLE ARE SOUGHT TO BE UNDERSTOOD DURING THE INAUGRAL FLIGHT.TRACKED TO THE LOST DETAIL BY AN ARRAY OF SOPHISTICATED COMPUTERS,IMPROVEMENT WILL BE INCPRPORATED FOR SUBSEQUENT FLIGHTS
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