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