Titan/Centaur D-1TTC-5 Helios B flight data report

Details Titan/Centaur D-1TTC-5 Helios B flight data report Titan/Centaur D-1TTC-5 Helios B flight data report

May 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976stin...7626254a&link_type=abstract

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Computer Science

Helios B, Interplanetary Trajectories, Launch Vehicles, Launch Windows, Centaur Launch Vehicle, Postflight Analysis, Solar Orbits, Tables (Data), Titan Launch Vehicles

Scientific paper

The fourth operational flight of the newest NASA unmanned launch vehicle is reported. The spacecraft was the Helios B, the second of two solar probes designed and built by the Federal Republic of Germany. The primary mission objective, to place the Helios spacecraft on a heliocentric orbit in the ecliptic plane with a perihelion distance of 0.29 AU, was successfully accomplished. After successful injection of the Helios spacecraft, a series of experiments were performed with the Centaur stage to demonstrate its operational capabilities. All objectives of the extended mission phase were successfully met. This report presents the analysis of the launch vehicle flight data for the primary mission phase of the TC-5 flight.

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