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1967-10-31
Standard
ARP767
This ARP provides design guidelines based on currently available information for the impact safety design of the cabin occupant environment.
1967-10-30
Technical Paper
670705
R. W. Sullivan
A low cost data acquisition and reduction system for an engine dynamometer laboratory is described. The system uses specially prepared Port-A-Punch data cards for input to a computerized data reduction program with the dynamometer operator functioning as an analog to digital converter.
1967-10-30
Technical Paper
670706
P. W. Callen
This paper describes three Allis-Chalmers' data acquisition systems showing the flexible points of each, and how the systems could be more flexible. These systems include a mobile system used for farm equipment testing, an 800 channel system used to collect test data from fuel cells, and a general purpose digital computer. Software support to process the data is also discussed.
1967-10-01
Standard
AS959
No scope available.
1967-10-01
Standard
AS960
No scope available.
1967-10-01
Standard
AS962
No scope available.
1967-10-01
Standard
AS961
No scope available.
1967-10-01
Standard
AS966
No scope available.
1967-10-01
Standard
AS964
No scope available.
1967-10-01
Standard
AS971
No scope available.
1967-10-01
Standard
AS972
No scope available.
1967-09-01
Magazine
1967-09-01
Standard
J1703_196709
This SAE Standard covers motor vehicle brake fluids of the nonpetroleum type for use in the braking system of any motor vehicle such as a passenger car, truck, bus, or trailer. These fluids are not intended for use under arctic conditions. These fluids are designed for use in braking systems fitted with rubber cups and seals made from styrene-butadiene rubber (SBR), or a terpolymer of ethylene, propylene, and a diene (EPDM).
1967-08-01
Standard
ARP997
The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish criteria for the installation of emergency equipment that shall permit its efficient use and encourage standardization, thereby reducing reorientation of crewmembers to equipment accessibility while working on differing types, models, and series of transport-category aircraft. This does not preclude the requirement to pre-flight check all emergency equipment relative to its location, availability, and operational status.
1967-08-01
Standard
J575D_196708
This SAE Recommended Practice is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances. This document provides standardized laboratory tests, test methods and equipment, and requirements for lighting devices covered by SAE Recommended Practices and Standards. It is intended for devices used on vehicles less than 2032 mm in width. Tests for vehicles larger than 2032 mm in overall width are covered in SAE J2139. Device specific tests and requirements can be found in applicable SAE technical reports.
1967-07-01
Standard
ARP435
This Aerospace Recommended Practice establishes performance standards for overspeed warning instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.4. This ARP covers an electro-mechanical pneumatic device which is calibrated to provide control contacts that can be made to operate a warning device whenever the indicated airspeed (IAS) reaches a maximum value as defined by the operating limit speed curve for the specific model aircraft.
1967-07-01
Standard
J994_196707
The scope of this SAE Standard is the definition of the functional, environmental, and life cycle test requirements for electrically operated backup alarm devices primarily intended for use on off-road, self propelled work machines as defined by SAE J1116 (limited to categories of 1) construction, and 2) general purpose industrial). This purpose of this document is to define a set of performance requirements for backup alarms, independent of machine usage. The laboratory tests defined in this document are intended to provide a uniform and repeatable means of verifying whether or nor a test alarm meets the stated requirements. For on-machine requirements and test procedures, refer to SAE J 1446.
1967-06-01
Standard
AS954
This SAE Aerospace Standard (AS) covers high strength thin wall (commercial) sockets, universal sockets, box wrenches and torque adaptors which possess the strength, clearances, and internal wrenching design so configured that, when mated with 12-point fasteners conforming to the requirement of AS870, they shall transmit torque to the fastener without bearing on the outer 5% of the fastener's wrenching points. Inclusion of dimensional data in this document is not intended to imply that all of the products described herein are stock production sizes. Consumers are requested to consult with manufacturers concerning lists of stock production sizes. The dimensional limits of box and combination wrench lengths have been established to provide configuration control for tool storage applications.
1967-05-15
Technical Paper
670512
Richard A. Muzechuk
Five test devices were developed to aid in the development of new friction materials. A friction machine has been equipped with disc brake apparatus and the data compared with standard drum friction machine data. A method has been developed which utilized fast response thermocouples to measure interface temperature distribution during dynamometer tests. Extremely high temperatures have been noted. Three laboratory tests were developed to evaluate brake materials' susceptibility to produce noise: vibration tests to measure dynamic characteristics; friction machine tests to measure negative damping; slip-stick machine tests which use the lining's noise producing tendency to excite a resonant system. Correlation of these tests with vehicle data were investigated and are discussed in the paper.
1967-05-15
Standard
ARP488
null, null
The purpose of this Aerospace Recommended Practice (ARP) is to provide design recommendations for passenger cabin entry doors, service doors, and emergency exits. The objective is to have a reliable system standardized to make operation of the exits simple, quick and obvious to all occupants under normal and emergency conditions and facilitate qualification of cabin attendants for different airplanes. NOTE: It is not the purpose of this ARP to specify the design method or specific mechanism to accomplish the objectives.
1967-05-01
Standard
J527A_196705
This SAE Standard covers brazed double wall low-carbon steel tubing intended for general automotive, refrigeration, hydraulic, and other similar applications requiring tubing of a suitable quality for bending, flaring, beading, forming, and brazing.
1967-04-01
Standard
AMS2355A
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought aluminum alloy and wrought magnesium alloy mill products (except forging stock), and includes quality assurance and testing procedures for rolled, forged, and flash welded rings (See 8.3). Requirements are specified in inch/pound units.
1967-04-01
Standard
AMS2635B
Primarily for determining the presence of cracks, porosity, blowholes, inclusions, and other imperfections which may or may not be exposed to the surface and which may be detrimental to usage of the parts.
1967-03-31
Standard
ARP899
This ARP establishes the basic test and design requirements for permanently attached tube fittings for use in aerospace fluid systems. Definitions of fitting and related terms are included in 6.3. This document recommends the tooling envelope, design criteria, and test requirements for tube fittings attached to tubing by methods which are usually considered to be permanent (brazing, welding, swaging, shrink fit, etc.).
1967-03-01
Standard
J594D_196703
This SAE Standard provides test procedures, requirements, and guidelines for reflex reflectors.
1967-02-01
Technical Paper
670583
David R. Reese
A description of the largest Acoustic and Vibration Test Facilities in existence for the simulation of major launch vehicle dynamic environment is given and the operational characteristics of both are discussed. Sinusoidal and random excitation techniques are described and unique vibration control methods presented. A comparison of the effects of vibration and acoustic excitation on major space vehicle structures is made.
1967-02-01
Technical Paper
670580
J. D. Stachiw
Simulated hydrospace is a valuable tool for the solution of engineering problems in the area of ocean engineering. It is employed not only in the research into the behavior of materials and structures under deep ocean environment but also in the quality control of industrial products for hydrospace market. Since a simulated hydrospace facility represents a considerable investment, it is important for all concerned in the decision making process for the acquiring of such a facility to understand the function that such a facility performs.
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