Accession Number : AD0332877
Title : Drag and Stability for the Pershing Nose Cone Obtained from Free-Flight Model Firings at Transonic to Hypersonic Velocities (Mach 1.06 to 9.26).
Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD
Personal Author(s) : CROGAN, LEONARD E.
Report Date : 03 SEP 1962
Pagination or Media Count : 4
Abstract : Range firings have been conducted using three sizes of PERSHING nose cone models to obtain drag and stability data at Mach numbers from 1.06 to 9.26. The models were found to be both statically and dynamically stable at the Mach numbers investigated. (Author)
Descriptors : *NOSE CONES, DRAG, SURFACE TO SURFACE MISSILES, HYPERSONIC CHARACTERISTICS, STABILITY.
Subject Categories : Surface-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE