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Technical Paper
1962-01-01
E. J. Briggs
Technical Paper
1962-01-01
F. J. Howland
Major in-service improvement programs in air traffic control are the high altitude area positive control expansion program and the terminal positive separation program. Both are in consonance with recommendations of the FAA Administrator's Task Force on air traffic control. The former will establish positive control in all U.S. airspace between 24,000 and 60,000 ft. A protoytpe terminal positive separation area will be established at Atlanta, Ga., in November 1962 to separate all aircraft within 15 miles of Atlanta between 2000 and 6000 ft. mean sea level. This will test the capability of the system to provide positive separation to all traffic operating within the designated airspace. This paper discusses the implementation of these systems.
Technical Paper
1962-01-01
Albert Brown
The proper use of the nation's airspace involves a large complex system which must function as an integrated unit. This paper deals with future automation of the air traffic control subsystem of this larger airspace utilization system. A detailed description of the data processing and display equipment and functions is given. The equipment which will be installed in air traffic control facilities permits the separation of advance planning and active control of aircraft. Reliability is enhanced by the use of several independent channels between data acquisition elements and the controller's display. This approach results in a system which will “fail softly.”
Technical Paper
1962-01-01
Jack W. Greweil
Interim developments which bridge the gap in ATC system improvements between immediate programs and the longer range objectives of the FAA's National Airspace utilization System Design are presented. The system design specifies that pilots and controllers shall have independent means of position determination. The national system of VORTAC/ILS aids which provide the position information used by pilots for this purpose is described, including an outline of the Acency's improvement plans in the next five years in this and the related field of air/ground communications. Radar and radar beacon are the independent source of aircraft position information for use by controllers. FAA plans for implementation of improved radar beacon interrogators, transponders, decoders, and procedures are described. The relationship of these developments with concurrent improvements being made at ATC display and processing equipments is noted.
Technical Paper
1962-01-01
R. H. Fredericks
Increased safety of today's automobiles is the direct result of simulated crash studies made by manufacturers and participated in by associated activities. This paper highlights the effectiveness of seat belts in minimizing injury to passengers and drivers. Other protective devices and improvements are also discussed in relation to the research program and continuing study of factors contributing to accident casualties.
Standard
1962-01-01
This recommended practice covers a series of stands that may be used for assembly, disassembly and maintenance; incorporating the following design criteria: a collapsible frame construction, envelope dimensions, attachment shear pad configuration and gear box and caster specifications. To provide a recommended practice for the design of a series of build-up stands which will be adaptable to small propulsion units (excluding those units requiring special assembly) and/or all propulsion unit components for the specified classes.
Technical Paper
1962-01-01
D. M. Severy, J. H. Mathewson, A. W. Siegel
Engineering methodology and research techniques, applied to 12 intersection-type automobile collision experiments, provided data on four speeds of impact and on three positions of impact. Anthropometric dummy motorists provide collision force and kinematic data for several conditions of restraint. Advanced photographic equipment identify new approaches to solution of the motorist collision injury problem. Specific data include tri-axial acceleration patterns for motorist head and chest and for car passenger compartment; identification of many factors associated with door latch failure and motorist ejection; demonstration of protection provided by the shoulder strap and lap belt combination; preliminary findings on tempered side window glass breakage and related head impact accelerations; collision dynamics and why modern car design has reduced probability for intersection collision roll-over; car collision deformation, skid patterns, and cost to repair damages are given for these controlled exposures.
Standard
1962-01-01
This Aerospace Recommended Practice provides criteria for design with respect to overall safety, particularly to afford minimum risk exposure to flight attendants and passengers from injuries due to: A. Routine use of galley installations B. Galley components becoming dislodged under routine or abnormal operating conditions and under survivable crash or ditching conditions C. Malfunctions of, or defects in, galleys or associated galley equipment. NOTE: It is not the purpose of this Aerospace Recommended Practice to specify the design methods or specific design to be followed in the accomplishment of the stated objectives.
Standard
1961-12-31
It is intended that this SAE Aerospace Recommended Practice (ARP) will set down guidelines for the development and test of gas motors to provide a practical and reliable hot gas rotary actuation mechanism. Specific operational and test requirements shall be specified in a detail specification.
Standard
1961-11-30
The following design features are provided by this recommended practice: 1. Prevention of installation of gyro in wrong position vector-wise. 2. Prevention of wrong gyro from being installed by use of a coded keying system. 3. Center of gravity mount. 4. Use of plug and socket type connectors rather than soldered terminals. 5. Self test feature. 6. Standard to be flexible enough to allow for expansion of types as the need arises. 7. A policed and controlled recommended practice. 8. Plug-in rate gyro. 9. Elimination of wrong harness connection by use of MS33683-1 standard which has 3 keyway positions. This could by expanding to 5 positions.
Technical Paper
1961-09-14
John Paul Stapp
This paper is a recap of this year's conference
Magazine
1961-09-01
Standard
1961-08-15
Air Condiitioning System - General - Dealing with Design Features. Air Conditioning Equipment - Commercial Passenger - Delaing with features. Applicable only to commercial passenger carrying aircraft. Desirable Design Features - General information for use of those concerned in meeting requirements contained herein.
Magazine
1961-08-01
Standard
1961-08-01
The purpose of this Report was to provide guidance to the commercial transport aviation industry in the selection and usage of oxygen equipment for high altitude transport aircraft. This Report reflects the consensus of views of the various parts of the industry contacted. The document is based on sound engineering and physiological principles and research data. The recommendations embodied in this document are applicable to commercial transport aircraft for operations between 8,000 and 40,000 ft. altitude.
Standard
1961-07-01
This specification covers a synthetic rubber in the form of soft wall, smooth bore, collapsing-type hose. This hose has been used typically for fueling aircraft from tank trucks or pits where the hose will be rolled flat for stowage on a reel, but usage is not limited to such applications. Not recommended for operating pressures higher than 125 psi (862 kPa).
Standard
1961-07-01
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 185 psi (1276 kPa).
Standard
1961-07-01
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 250 psi (1724 kPa).
Standard
1961-06-01
This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows: type I: ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. Type II: millivoltmeter type, operated and actuated by varying EMF output of a thermocouple; the varying EMF input to the instrument being obtained by temperature changes of the temperature sensing thermocouple. This document establishes the essential minimum safe performance standards for electrical type temperature instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4.
Standard
1961-06-01
This document includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a) single engine personal and/or liaison type; b) light twin engine; c) large multiengine propeller; d) large multiengine turbojet; e) military high performance fighter and attack; and f) helicopter. The purpose of this document is to provide certain basic considerations and design criteria for installation of landing and taxiing light systems for night operation.
Standard
1961-05-01
This Aeronautical Standard establishes the essential minimum safe requirements for pitot-static type of Maximum Allowable Airspeed Instruments primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the instruments to the environmental conditions specified in paragraph 3.3. This Aeronautical Standard covers the basic types of maximum allowable airspeed instruments which give a continuous indication of both indicated air speed and maximum allowable airspeed not exceeding 650 knots.
Standard
1961-04-01
This Aerospace Recommended Practice (ARP) provides recommendations intended for standardization of safety lap belts without hindering the development of new, improved design. The purpose is not to specify the design methods or specific mechanism to accomplish the objectives.
Standard
1961-04-01
This Aeronautical Standard establishes the essential minimum safe performance standards for Fuel and Oil Quantity Instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instrument to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers the capacitance sensor type of instrument.
Standard
1961-04-01
This SAE Standard may be used for all revolving cranes wherein the capacity of the crane to support loads is based on its resistance to overturning. it is not applicable to cranes wherein the capacity of the crane is based on structural strength or available hoisting power. The purpose of this test is to determine the maximum capacity of a crane to counterbalance loads applied on its hook block. The capacity of the crane is reported in terms of the load in kilograms (pounds) and its corresponding radius in meters (feet) for a specified position of the upperstructure with respect to the mounting.
Magazine
1961-02-01
Technical Paper
1961-01-01
K.A. Stonex
Magazine
1960-12-01
Standard
1960-11-15
No scope available.
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