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INSAT-1A launch on DeltaThe INSAT-1A, the first in a series of 12 transponder communications satellites developed for India, is described as well as the launch plans. The launch vehicle will be the Delta 3910 configuration which incorporates an extended long tank Thor booster, nine Castor IV strap-on motors, a TR-201 second stage, and an 8 foot fairing. The satellite will be placed in a suborbital trajectory. A DAM-D stage will then thrust it into a synchronous transfer orbit. An apogee kick motor will be fired to circularize its orbit at a geosynchronous altitude of 19,300 nautical miles.
Document ID
19820013357
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Astronautics (General)
Report/Patent Number
NASA-TM-84159
NAS 1.15:84159
REPT-0-492-214-82-1
Report Number: NASA-TM-84159
Report Number: NAS 1.15:84159
Report Number: REPT-0-492-214-82-1
Accession Number
82N21231
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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