Accession Number:

AD0627663

Title:

STABILITY AND DRAG OF A MODIFIED SATURN/APOLLO SECOND-STAGE CONFIGURATION IN THE NOL PRESSURIZED BALLISTICS RANGE.

Descriptive Note:

Final test rept.,

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

Report Date:

1965-11-04

Pagination or Media Count:

22.0

Abstract:

Thirty launchings of models of a modified SaturnApollo second-stage configuration were performed. The purpose of the launchings was to obtain stability and drag coefficients in a realm of Mach numbers from 4 to 8 and ambient air pressures from 6.3 to 928 mm Hg. Author

Subject Categories:

  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE