NDLI: The rca-f/delta launch

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The rca-f/delta launch

Content Provider	NASA Technical Reports Server (NTRS)
Copyright Year	1983
Description	The Delta 3924 launch vehicle configuration which incorporates the extended long tank Thor booster, nine Castor 4 strap-on motors, the AJ-118 second stage and the TE 364-4 third stage is to place into a synchronous transfer orbit, the second in a series of high-traffic capacity, 24 transponder communications satellites. Three days after launch, the satellite's apogee kick motor circularizes the orbit at geosynchronous altitude of 19,300 NM above the equator at approximately 128 degrees W longitude. The satellite can service commercial and government voice, digital and video communications requirements between Alaska and CONUS. The communications payload, mission requirements and spacecraft systems and subsystems are described.
File Size	2935019
Page Count	32
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19830012718
Archival Resource Key	ark:/13960/t52g2jv1p
Language	English
Publisher Date	1983-03-31
Access Restriction	Open
Subject Keyword	Launch Vehicles And Space Vehicles Delta Launch Vehicle Domestic Satellite Communications Systems Apogee Boost Motors Transfer Orbits Launch Vehicle Configurations Satellite Configurations Rca Satcom Satellites Spacecraft Launching Prelaunch Summaries Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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