Display:

Results

Viewing 22231 to 22260 of 23354
1966-02-01
Technical Paper
660694
R. W. Gray
Automation of high production, high complexity, and high speed testing is often of obvious worth. The use of automation by the “popular” space programs has developed techniques that warrant consideration of systems previously considered to be incompatible with automatic testing, either because of testing difficulty or cost. Manual testing is still a requirement in the developmental testing phase of many programs. It is also an established requirement in many factory level tests. The complete systems approach involving the total mission requirements for factory through launch (or other use) sequence will enable the logical selection of the correct testing elements, both automatic and manual.
1966-02-01
Technical Paper
660121
E. J. Hughes, G. O. Boston, P. A. Diddens
A new method of testing Automatic Transmission Main Control Assemblies has been developed which provides increased reliability in transmission valve body testing. This method employs an electro-hydraulic test stand sequenced by an IBM 1710 computer system. The computer controls the test cycle, accurately compares test values against test specification parameters, records all test values, and determines whether the transmission Main Control meets all specifications.
1966-02-01
Technical Paper
660095
Jose L. Bascunana, Lewis D. Conta
Research on charge stratification of spark ignition engines has been under way at the University of Rochester for some time. Most recently the successful propane burning engine previously reported before the SAE has been converted to liquid fuel operation. This paper discusses some of the problems involved in the conversion and presents the results of tests on the liquid fuel version of the engine.
1966-01-01
Magazine
1965-11-01
Standard
AIR910
The purpose of this report is to provide information on ozone and its control in high altitude aircraft environmental systems. Sources of this information are listed in the selected bibliography appearing at the end of this report, to which references are made throughout.
1965-11-01
Magazine
1965-10-20
Technical Paper
650959
R. G. RIESER, G. E. MICHAELS
1965-10-20
Technical Paper
650964
EARL R. SMITH
1965-10-15
Standard
AIR787
This Aerospace Information Report provides technical information to assist the development of specific cleaning methods for filter elements. Consideration is limited to filter elements which are designated as 'cleanable' (not 'disposable'), but which cannot be cleaned by simple and obvious procedures. Cleaning methods developed according to this report should be evaluated by the methods of ARP 725 and ARP 849. Satisfactory cleaning methods can be developed for most 'cleanable' filter elements. Technical or economic feasibility of the cleaning method may be limited, however, by incompatibility of filter-element construction materials, by mechanical weakness or lack of corrosion resistance to withstand repeated or continued cleaning, or by the presence of unusually tenacious contamination. These factors must be considered when selecting approaches to the development of specific methods.ic methods.ic methods.ic methods.
1965-10-01
Standard
ARP881
This SAE Aerospace Recommended Practice (ARP) lists the lamps in Table 1 that are recommended for the type of service indicated. This list is not intended as a catalog and does not include many types that are now in use. This specification is not applicable to Solid State Lighting Lamp Assemblies (Based LED lamps). It does, however, reflect current practice.
1965-10-01
Magazine
1965-09-01
Standard
AMS3380A
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid. Primarily for fluid lines operating in service up to 230 degrees C (446 degrees F) and under pressures up to 1500 psi (10,342 kPa).
1965-09-01
Standard
AMS3159A
This specification covers a liquid oxygen compatible gas-leak deteching compound in the form of a liquid.
1965-09-01
Standard
J843A_196509
This SAE Recommended Practice establishes a uniform procedure for the level road test of the brake systems of new light-duty trucks and new multipurpose passenger vehicles up to and including 2700 kg (6000 lb) GVW and all classes of new passenger cars. The purpose of the test code is to establish brake system capabilities with regard to: a. Deceleration versus input, as affected by vehicle speed, brake temperature, and usage; b. brake system integrity; c. Stopping ability during emergency or inoperative power assist conditions; d. Water recovery characteristics.
1965-09-01
Standard
AMS2355
null, null
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.
1965-09-01
Magazine
1965-08-01
Standard
AS406
This standard establishes the essential minimum safe performance requirements for flight director instruments, primarily for use with turbine-powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.3. This standard covers flight directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a preselected flight plan.
1965-07-30
Standard
AIR805A
The purpose of this information report is to present factors which affect the design and development of jet blast windshield rain removal systems for commercial transport aircraft. A satisfactory analytical approach to the design of these systems has not yet been developed. Although detailed performance data are available for some test configurations, rain removal systems will generally be unique to specific aircraft. This, then, requires a preliminary design for the system based on available empirical data to be followed with an extensive laboratory development program.
1965-07-01
Standard
J823A_196507
This SAE Standard specifies the test procedure, test circuitry, and instruments required for measuring the performance of flashers used in motor vehicles.
1965-07-01
Standard
J575B_196507
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.
1965-07-01
Magazine
1965-06-01
Standard
ARP798
The purpose of this document is to recommend to the designer the various criteria, and to familiarize him with techniques, associated with white incandescent lighted aerospace instruments. This recommended practice covers the general requirements and test procedures recommended for use with white incandescent integrally lighted instruments. Its use should provide uniformity of illumination from instrument to instrument and legibility under daylight operation. An appendix is provided to familiarize the designer with some of the techniques used to obtain uniformity of color and illumination in various types of instruments.
1965-06-01
Magazine
1965-05-01
Standard
ARP712
This SAE Aerospace Recommended Practice (ARP) provides minimum standards and environmental design requirement recommendations for lighting and control in galley areas. It also addresses electrical shock hazard in galley areas. The purpose of this recommended practice is to provide minimum standards for the illumination of galleys (buffets) and for the location of lighting controls within the galley area of passenger transport aircraft.
1965-05-01
Magazine
1965-04-20
Standard
ARP750
The purpose of this Aerospace Recommended Practice (ARP) is to provide design criteria that will lead to seat designs which provide maximum safety for air transportation passengers. It is not the purpose of this ARP to specify design methods or specific designs to be followed in the accomplishment of the stated objectives.
1965-04-01
Standard
AIR883
(This document supersedes and cancels AIR 12) 'Ground resonance' is a term which originated in the early days of autogiro development in this country. It is a somewhat ambiguous term as the conditions it describes usually occur at the ground but do not have any association with the common expression 'ground effect'. However, the troubles usually associated with 'ground resonance' do occur when the ship is on or near the ground.
1965-02-10
Standard
ARP846
The purpose of these specifications is to provide a standard procedure and standard equipment for the evaluation of a measurement of the ionization voltage (sparking voltage) of shunted surface gap spark igniter designs. These specifications contain general information pertaining to the sparking voltage parameter of shunted surface gap spark igniters; test equipment circuitry; bill of materials for test equipment; test equipment operation.
1965-02-01
Technical Paper
650264
H. V. Borst
A new vertical take-off and landing aircraft, designated the X-19, has been built with high load carrying capacity, high cruise-speed, and extended hover capability. It is a tandem-wing, tilt-propeller vehicle powered by two turbo-shaft engines. The design meets the exacting performance, stability, and control requirements of hover and low-speed flight while maintaining high transport efficiency at cruise. The basic elements of the design are suitable for a series of new operating requirements for military and civil uses. The flight test results of the X-19 confirm the performance and handling predictions and, thus, prove that desired operating characteristics of V/STOL aircraft can be obtained.
1965-02-01
Technical Paper
650258
B. D. Sissom
One purpose of the Army’s reorganization in 1962 was to consolidate and streamline testing of its materiel. Objectives of the Army’s new test organization, the Test and Evaluation Command, are briefly discussed. The scope of testing on military vehicles, including test planning, type of tests conducted facilities used, and reporting procedures, are outlined. Evaluation of test results is compared against military requirements.
Viewing 22231 to 22260 of 23354

Filter