Computer Science – Performance
Scientific paper
Mar 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992icss.conf..580h&link_type=abstract
IN: AIAA International Communication Satellite Systems Conference and Exhibit, 14th, Washington, DC, Mar. 22-26, 1992, Technical
Computer Science
Performance
Commercial Spacecraft, Earth Orbital Environments, Spacecraft Performance, Titan 3 Launch Vehicle, Launch Vehicle Configurations, Payload Integration, Project Planning
Scientific paper
This paper will address the Titan III launch vehicle performance capabilities for missions to Low Earth Orbit and InterPlanetary Orbits. Throw-weight capability into these types of orbits will be addressed from a launch vehicle-only perspective as well as launch vehicle/upper stage combinations. Performance, mission design, and constraints for a single satellite configuration will be examined, along with interface (physical and functional), and ground/flight operations requirements for a Cape Canaveral launch for both single and dual satellite configurations. Martin Marietta's success rates have shown very high reliability for all its Titan configurations.
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