Phonocardiograph microphone is rugged and moistureproof

Microphone used as a phonocardiograph transducer monitors small amplitude audio signals in the presence of large shock loads and high humidity. It contains a lead zirconate-lead titanate piezoelectric plate encapsulated in a flexible polyurethane resin. The resin is contained in a sealed nylon case having a diameter of less than one inch

Phonocardiograph transducer Patent

Piezoelectric transducer for monitoring sound waves of physiological origi

Fixed-Base Simulator Studies of the Ability of the Human Pilot to Provide Energy Management Along Abort and Deep-Space Entry Trajectories

A simulation study has been made to determine a pilot's ability to control a low L/D vehicle to a desired point on the earth with initial conditions ranging from parabolic orbits to abort conditions along the boost phase of a deep-space mission. The program was conducted to develop procedures which would allow the pilot to perform the energy management functions required while avoiding the high deceleration or skipout region and to determine the information display required to aid the pilot in flying these procedures. The abort conditions studied extend from a region of relatively high flight-path angles at suborbital velocities while leaving the atmosphere to a region between orbital and near-escape velocity outside the atmosphere. The conditions studied included guidance from suborbital and superorbital aborts as well as guidance following return from a deepspace mission. In this paper, the role of the human pilot?s ability to combine safe return abort procedures with guidance procedures has been investigated. The range capability from various abort and entry conditions is also presented

Apparatus for measuring an aircraft's speed and height

An apparatus for measuring aircraft horizontal speed and height above ground without the need for airborne cooperative devices is presented. Two ground level TV cameras separated by a measured distance and pointed at zenith are placed in line with the projection of the expected path of the aircraft. Speed is determined by measuring the time that it takes the aircraft to travel between the fields of view of the two TV cameras using zenith crossings as the reference points. Height is determined by correlating the speed with the time required to cross the field of view of either of the two cameras

A method for measuring aircraft height and velocity using dual television cameras

A unique electronic optical technique, consisting of two closed circuit television cameras and timing electronics, was devised to measure an aircraft's horizontal velocity and height above ground without the need for airborne cooperative devices. The system is intended to be used where the aircraft has a predictable flight path and a height of less than 660 meters (2,000 feet) at or near the end of an air terminal runway, but is suitable for greater aircraft altitudes whenever the aircraft remains visible. Two television cameras, pointed at zenith, are placed in line with the expected path of travel of the aircraft. Velocity is determined by measuring the time it takes the aircraft to travel the measured distance between cameras. Height is determined by correlating this speed with the time required to cross the field of view of either camera. Preliminary tests with a breadboard version of the system and a small model aircraft indicate the technique is feasible

Research and development of materials for use as lubricants in a liquid hydrogen environment Final report, Jul. 1964 - Nov. 1965

Lubricant materials for rolling contact bearings operating in liquid hydrogen environmen

Research study of an aircraft-contained radar zero-zero landing system, volume 1 Final report, Jan. - Dec. 1967

Two rapid scan radar/display techniques evaluated for use in aircraft-contained zero-zero landing syste

Closed-cycle gas dynamic laser design investigation

A conceptual design study was made of a closed cycle gas-dynamic laser to provide definition of the major components in the laser loop. The system potential application is for long range power transmission by way of high power laser beams to provide satellite propulsion energy for orbit changing or station keeping. A parametric cycle optimization was conducted to establish the thermodynamic requirements for the system components. A conceptual design was conducted of the closed cycle system and the individual components to define physical characteristics and establish the system size and weight. Technology confirmation experimental demonstration programs were outlined to develop, evaluate, and demonstrate the technology base needed for this closed cycle GDL system

Research study of an aircraft-contained radar zero-zero landing system, volume 2 Final report, Jan. - Dec. 1967

Conceptual development of long wave radar display based on processed plan position indicator and cross beam raster scan technique

Bonding Alone: Familism, Religion, and Secular Civic Participation

This study examines the influence of familism, religion, and their interaction on participation in secular voluntary associations. We develop an insularity theory to explain how familism and religion encourage Americans to avoid secular civic participation. Using data from the first wave of the National Survey of Families and Households, this study finds that familism reduces participation in secular organizations. Moreover, religion moderates the effect of familism: specifically, religious involvement tends to increase the negative effect of familism on secular civic participation. Although religious involvement in and of itself fosters secular civic participation, strong familism tends to dampen positive impacts of religious involvement. For familistic individuals, religious congregations appear to reinforce their insularity within their immediate social circle and family