Original is a photocopy; W. A. Wilson, Chairman; Russell Meredith, North American Aviation; Robert Hackman, Linde Company; Frank Wallace, Pratt-Whitney Aircraft; P.G. Parks, NASA, MSFC; G. O. Hoglund, Aluminum Company of America.
Cryogenic propellant rocket engine hardware and the related test facilities will be described. Methods used for selection of alloys for liquid oxygen and liquid hydrogen service will be discussed. Unique equipment and welding procedures are reviewed with emphasis on welding problems and their solutions to assure reliable hardware and facilities. Examples of specific welding procedures and methods of quality assurance will be given for joining application ranging in size from .001" to 11" thick sections.
This document contains copies of management charts and photographs maintained in the Management Information Office of the Executive Staff on Advanced Program and Research and Technology Areas.
Konrad, Klaus, Ingeborg, and Betty Dannenberg and little George visit Cape Canaveral. On the film they are shown touring the NASA spaceflight facilities here, driving past a number of launching vehicles and pads. The film wraps up by showing a plaque commemorating the success of the Mercury spaceflight program. Fall 1967.
This paper presents representative examples of vibration and acoustic data from flights of the Saturn V launch vehicle and static firings of Saturn V launch vehicle stages. The purpose of the paper is to provide vibration and acoustic environment characteristics which are pertinent to the design of launch vehicles
