Moving refs out of templates
imported>Ohsin (Restored revision 1038435587 by 117.217.1.250 (talk): Reverting clumsy edits) |
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|SI = {{convert|253|isp}} | |SI = {{convert|253|isp}} | ||
|burntime = 49 seconds | |burntime = 49 seconds | ||
|fuel = PBAN ([[Polybutadiene acrylonitrile]]) [[Solid rocket|Solid]]<ref name=ISRO | |fuel = PBAN ([[Polybutadiene acrylonitrile]]) [[Solid rocket|Solid]]<ref name=ISRO/> | ||
|propmass = {{cvt|8.6|t|lb}} | |propmass = {{cvt|8.6|t|lb}} | ||
|thrust = {{cvt|46|tf|kN lbf|order=out}} | |thrust = {{cvt|46|tf|kN lbf|order=out}} | ||
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The first launch of the SLV took place in [[Sriharikota]] on 10 August 1979. The fourth and final launch of the SLV took place on 17 April 1983. | The first launch of the SLV took place in [[Sriharikota]] on 10 August 1979. The fourth and final launch of the SLV took place on 17 April 1983. | ||
It has taken approximately seven years to realise the vehicle from start. The solid motor case for first and second stage are fabricated from 15 CDV6 steel sheets and third and fourth stages from fibre reinforced plastic.<ref name=ISRO/> | It has taken approximately seven years to realise the vehicle from start. The solid motor case for first and second stage are fabricated from 15 CDV6 steel sheets and third and fourth stages from fibre reinforced plastic.<ref name=ISRO>{{cite web|url=https://www.isro.gov.in/sites/default/files/flipping_book/58-SI-Jul-Sep-05/files/assets/common/downloads/publication.pdf|title=First Successful Launch of SLV-3 - Silver Jubilee|publisher=ISRO}}</ref> | ||
== Launch statistics == <!-- Update after every launch --> | == Launch statistics == <!-- Update after every launch --> | ||