Accession Number : AD0850091
Title : Exploratory Development for Missile Guidance and Airframes.
Descriptive Note : Quarterly progress rept. 1 Oct-31 Dec 68,
Corporate Author : JOHNS HOPKINS UNIV LAUREL MD APPLIED PHYSICS LAB
Personal Author(s) : Noyes, C. F. ; Nagy, A. W. ; Amick, J. L. ; Weiss, R. O. ; Cramer, R. H.
Report Date : 1968
Pagination or Media Count : 21
Abstract : In this volume results are reported on work in the following categories: microelectronics laboratory improvements; maser research program; a maximum-deflection theory for two-dimensional jet interaction; high temperature effects on leading edge structures and materials; the allowable roughness on an aerodynamic surface without drag penalty; vibration studies; and a computer program for designing transpiration cooling systems. (Author)
Descriptors : (*NAVAL RESEARCH, GUIDED MISSILES), AERODYNAMIC CONFIGURATIONS, MICROELECTRONICS, MASERS, AIRFRAMES, REENTRY VEHICLES, EVAPOTRANSPIRATION, AERODYNAMIC HEATING, AERODYNAMIC CHARACTERISTICS, VIBRATION, COMPUTER PROGRAMMING, LEADING EDGES, STRUCTURAL PROPERTIES, COMPUTER PROGRAMMING.
Subject Categories : Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE