Accession Number : AD0843812

Title :   Range Safety Trajectory and Dispersion Information for the Atlas-Centaur Vehicle No. 1,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Bleitz, L.

Report Date : 02 JAN 1962

Pagination or Media Count : 22

Abstract : This report is an addendum to AE61-1219, RANGE SAFETY TRAJECTORY AND DISPERSION INFORMATION FOR THE ATLAS CENTAUR VEHICLE NO. 1., 8 December 1961. Since that date, certain flight parameters have been changed. Although the new trajectory remains within the bounds of the 30 dispersions, it was deemed prudent to rerun at least the nominal trajectory with the standard range safety data tabulations including premature cut-off data. (Author)

Descriptors :   *GUIDED MISSILE SAFETY), (*LAUNCH VEHICLES, FLIGHT TESTING), (*GUIDED MISSILE RANGES, ASCENT TRAJECTORIES, DESCENT TRAJECTORIES, FREE FLIGHT TRAJECTORIES, GUIDED MISSILE COMPONENTS, SCATTERING, DRAG, STAGING, MISS DISTANCE, IMPACT PREDICTION.

Subject Categories : Safety Engineering
      Spacecraft Trajectories and Reentry
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE