Accession Number:

AD0843812

Title:

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

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Bleitz, L.

Report Date:

1962-01-02

Pagination or Media Count:

22.0

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 Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE