�ݺ�ߣshows by User: saamleoprasad

�ݺ�ߣshows by User: saamleoprasad / http://www.slideshare.net/images/logo.gif �ݺ�ߣshows by User: saamleoprasad / Fri, 11 Jul 2014 06:01:37 GMT �ݺ�ߣShare feed for �ݺ�ߣshows by User: saamleoprasad Indian satellite lunch vehicles /saamleoprasad/indian-satellite-lunch-vehicles indiansatellitelunchvehicles-140711060137-phpapp01
Geosynchronous Satellite Launch Vehicle(GSLV) ,is capable of placing INSAT–II class of satellites (2000 – 2,500 kg) into Geosynchronous Transfer Orbit (GTO). GSLV is a three stage vehicle GSLV is 49 m tall, with 414 t lift off weight. It has a maximum diameter of 3.4 m at the payload fairing. First stage comprises S125 solid booster with four liquid(L40) strap–ons . Second stage (GS2) is liquid engine and the third stage (GS3) is a cryo stage. The vehicle develops a lift off thrust of 6573 kn. The first flight of GSLV took place from SHAR on April 18, 2001 by launching 1540 kg GSAT-1. It was followed by six more launches , GSLV-D2 on May 8, 2003 (GSAT-2 1825 kg), GSLV-F01 on September 20, 2004 (EDUSAT 1950 kg), GSLV-F02 on July 10, 2006, GSLV-F04 on September 2, 2007 (INSAT-4CR 2130 kg), GSLV-D3 on April 15, 2010, GSLV-F06 on December 25, 2010 and GSLV-D5 on January 05, 2014 (GSAT-14 1982 kg). ]]>
Geosynchronous Satellite Launch Vehicle(GSLV) ,is capable of placing INSAT–II class of satellites (2000 – 2,500 kg) into Geosynchronous Transfer Orbit (GTO). GSLV is a three stage vehicle GSLV is 49 m tall, with 414 t lift off weight. It has a maximum diameter of 3.4 m at the payload fairing. First stage comprises S125 solid booster with four liquid(L40) strap–ons . Second stage (GS2) is liquid engine and the third stage (GS3) is a cryo stage. The vehicle develops a lift off thrust of 6573 kn. The first flight of GSLV took place from SHAR on April 18, 2001 by launching 1540 kg GSAT-1. It was followed by six more launches , GSLV-D2 on May 8, 2003 (GSAT-2 1825 kg), GSLV-F01 on September 20, 2004 (EDUSAT 1950 kg), GSLV-F02 on July 10, 2006, GSLV-F04 on September 2, 2007 (INSAT-4CR 2130 kg), GSLV-D3 on April 15, 2010, GSLV-F06 on December 25, 2010 and GSLV-D5 on January 05, 2014 (GSAT-14 1982 kg). ]]> Fri, 11 Jul 2014 06:01:37 GMT /saamleoprasad/indian-satellite-lunch-vehicles saamleoprasad@slideshare.net(saamleoprasad) Indian satellite lunch vehicles saamleoprasad Geosynchronous Satellite Launch Vehicle(GSLV) ,is capable of placing INSAT–II class of satellites (2000 – 2,500 kg) into Geosynchronous Transfer Orbit (GTO). GSLV is a three stage vehicle GSLV is 49 m tall, with 414 t lift off weight. It has a maximum diameter of 3.4 m at the payload fairing. First stage comprises S125 solid booster with four liquid(L40) strap–ons . Second stage (GS2) is liquid engine and the third stage (GS3) is a cryo stage. The vehicle develops a lift off thrust of 6573 kn. The first flight of GSLV took place from SHAR on April 18, 2001 by launching 1540 kg GSAT-1. It was followed by six more launches , GSLV-D2 on May 8, 2003 (GSAT-2 1825 kg), GSLV-F01 on September 20, 2004 (EDUSAT 1950 kg), GSLV-F02 on July 10, 2006, GSLV-F04 on September 2, 2007 (INSAT-4CR 2130 kg), GSLV-D3 on April 15, 2010, GSLV-F06 on December 25, 2010 and GSLV-D5 on January 05, 2014 (GSAT-14 1982 kg). <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/indiansatellitelunchvehicles-140711060137-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds" /><br> Geosynchronous Satellite Launch Vehicle(GSLV) ,is capable of placing INSAT–II class of satellites (2000 – 2,500 kg) into Geosynchronous Transfer Orbit (GTO). GSLV is a three stage vehicle GSLV is 49 m tall, with 414 t lift off weight. It has a maximum diameter of 3.4 m at the payload fairing. First stage comprises S125 solid booster with four liquid(L40) strap–ons . Second stage (GS2) is liquid engine and the third stage (GS3) is a cryo stage. The vehicle develops a lift off thrust of 6573 kn. The first flight of GSLV took place from SHAR on April 18, 2001 by launching 1540 kg GSAT-1. It was followed by six more launches , GSLV-D2 on May 8, 2003 (GSAT-2 1825 kg), GSLV-F01 on September 20, 2004 (EDUSAT 1950 kg), GSLV-F02 on July 10, 2006, GSLV-F04 on September 2, 2007 (INSAT-4CR 2130 kg), GSLV-D3 on April 15, 2010, GSLV-F06 on December 25, 2010 and GSLV-D5 on January 05, 2014 (GSAT-14 1982 kg).

Indian satellite lunch vehicles from Samaleswari Prasad Mallik

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0 Fixed wing aircrafts power point presentation /slideshow/fixed-wing-aircrafts-power-point-presentation/34315065 fixedwingaircraftspowerpointpresentation-140505204636-phpapp01
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]]> Mon, 05 May 2014 20:46:36 GMT /slideshow/fixed-wing-aircrafts-power-point-presentation/34315065 saamleoprasad@slideshare.net(saamleoprasad) Fixed wing aircrafts power point presentation saamleoprasad <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/fixedwingaircraftspowerpointpresentation-140505204636-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds" /><br>

Fixed wing aircrafts power point presentation from Samaleswari Prasad Mallik

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0 https://cdn.slidesharecdn.com/profile-photo-saamleoprasad-48x48.jpg?cb=1571549509 https://cdn.slidesharecdn.com/ss_thumbnails/indiansatellitelunchvehicles-140711060137-phpapp01-thumbnail.jpg?width=320&height=320&fit=bounds saamleoprasad/indian-satellite-lunch-vehicles Indian satellite lunch... https://cdn.slidesharecdn.com/ss_thumbnails/fixedwingaircraftspowerpointpresentation-140505204636-phpapp01-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/fixed-wing-aircrafts-power-point-presentation/34315065 Fixed wing aircrafts p...