STABILITY AND DRAG OF A MODIFIED SATURN/APOLLO SECOND-STAGE CONFIGURATION IN THE NOL PRESSURIZED BALLISTICS RANGE.
Abstract
Thirty launchings of models of a modified Saturn/Apollo 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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 04, 1965
- Accession Number
- AD0627663
Entities
People
- David N. Bixler
- Stuart L. Hanlein
Organizations
- Naval Ordnance Laboratory