Find the standard you are looking for at Engineering360. Documents are available for purchase from the IHS Standards Store.

1 - 20 of 25 results

NAVY - MIL-C-39024/6C - CONNECTOR, ELECTRICAL, TEST POINT TYPE, PRINTED WIRING, 4 AND 8 TEST POINT, (CENTER MOUNTING) 0.156 INCH CONTACT SPACING Organization: NAVY
Date: 1971-12-20
NR - BRS-SM 523 ISSUE F - RAIL CLAMP POINT LOCK CENTRE THRUST BRACKET ASS'Y TYPE A (ACTUATOR MOUNTING) Organization: NR
Date: 1989-06-02
NR - BRS-SM 524/2 ISSUE A - RAIL CLAMP POINT LOCK CENTRE THRUST BRACKET ASSEMBLY TYPE B2 (ACTUATOR MOUNTING) Organization: NR
Date: 1990-09-12
NR - BRS-SM 524 ISSUE D - RAIL CLAMP POINT LOCK CENTRE THRUST BRACKET ASSEMBLY TYPE B1 (ACTUATOR MOUNTING) Organization: NR
Date: 1989-06-08
NR - BRS-SM 2252/1 - RAIL CLAMP POINT LOCK D/A THROUGH ROD CYLINDER CENTRE BOSS MOUNTED Organization: NR
Date: 1985-11-12
SAE J2133 - DISC WHEEL RADIAL RUNOUT LOW POINT MARKING Organization: SAE
Date: 2011-03-01
Description: This SAE Recommended Practice provides for standardized steel disc wheel radial runout low point marking. This marking is used for match-mounting tires on wheels to minimize assembly radial force variation.
SAE J2338 - RECOMMENDATIONS OF THE SAE TASK FORCE ON HEADLAMP MOUNTING HEIGHT Organization: SAE
Date: 2011-02-01
Description: The SAE International task force on headlamp mounting height has considered the ramifications of reducing the maximum mounting height of headlamps on highway vehicles.
IPC-7351 - GENERIC REQUIREMENTS FOR SURFACE MOUNT DESIGN AND LAND PATTERN STANDARD - INCLUDES CD-ROM; SUBSCRIPTION CUSTOMERS CAN OBTAIN ONE COMPLIMENTARY COPY FROM IHS BY CONTACTING IHS CUSTOMER CARE AT +1 800 IHS-CARE (+1 800 447-2273) OR VISIT WWW.IHS.COM/CUSTOMERCARE; INCLUDES ACCESS TO ADDITIONAL CONTENT Organization: IPC
Date: 2010-06-01
Description: *Fine-Pitch Technology (FPT) – A surface-mount assembly technology with component terminations on less than 0.625 mm [0.025 in] centers.*Fiducial (Mark) – A printed board artwork feature(s) that is created in the same process as the conductive pattern and that provides a common measurable point for component mounting with respect to a land pattern or land patterns.
NPFC - MIL-M-24359 - METERS, MILLIMETERS, DIRECT CURRENT PANEL MOUNTING (EDGEWISE TYPES) Organization: NPFC
Date: 1969-02-05
Description: Where the letter "R" is used in this group, between two figures, it represents a decimal point. Example: 1R5 represents 1.5. The full-scale value of zero-center or offset zero meters is indicated by two numbers designating the numerical value of the end-scale points, with a letter between them designating the decimal value of the numbers, as follows: D - tenths Example: 5D5 represents 0.5-0-0.5 U - units Example: 1U9 represents 1-0-9.
ASTM F1529 - STANDARD TEST METHOD FOR SHEET RESISTANCE UNIFORMITY EVALUATION BY IN-LINE FOUR-POINT PROBE WITH THE DUAL-CONFIGURATION PROCEDURE Organization: ASTM
Date: 2002-12-10
Description: Further, automatic instruments on which this test method will be performed may not have perfect centering of the wafer on the measurement stage. These factors require that the periphery of the layer being measured be excluded.
NASA-TR-R-433 - EXPERIMENTAL DETERMINATION OF AIRPLANE MASS AND INERTIAL CHARACTERISTICS Organization: NASA
Date: 1974-01-01
Description: Current practices are evaluated for experimentally determining airplane center of gravity, moments of inertia, and products of inertia.
ISO 16840-3 - WHEELCHAIR SEATING - PART 3: DETERMINATION OF STATIC, IMPACT AND REPETITIVE LOAD STRENGTHS FOR POSTURAL SUPPORT DEVICES - SECOND EDITION; CORRECTED VERSION: 09/01/2015 Organization: ISO
Date: 2014-01-15
Description: The maximum offset distance to the centre of the PSD from the adjacent attachment point can also be considered.
SNZ AS/NZS ISO 16840.3 - WHEELCHAIR SEATING PART 3: DETERMINATION OF STATIC, IMPACT AND REPETITIVE LOAD STRENGTHS FOR POSTURAL SUPPORT DEVICES Organization: SNZ
Date: 2015-10-02
Description: The maximum offset distance to the centre of the PSD from the adjacent attachment point can also be considered.
SAE J826 - DEVICES FOR USE IN DEFINING AND MEASURING VEHICLE SEATING ACCOMMODATION Organization: SAE
Date: 2015-11-01
Description: Additional considerations are necessary when a Head Restraint Measuring Device (HRMD) is mounted to an H-point machine (Appendix D). Purpose This document specifies a two-dimensional H-point template and a three-dimensional H-Point Machine (HPM) for use in defining and measuring accommodation in vehicle seats.
ESDU 76003 - GEOMETRICAL PROPERTIES OF CRANKED AND STRAIGHT-TAPERED WING PLANFORMS Organization: ESDU
Date: 2012-05-01
Description: For the special case of the straight-tapered wing, curves give the lengths of the chords and their quarter chord position as a function of taper ratio, centre-line chord, aspect ratio, and quarter-chord sweep.
SAE/TP - 2007-01-3874 - AUTOMATIC CONTROL IMPLEMENTATION AND UPGRADED ELECTRICAL SYSTEM DESIGN FOR THE OCULUS 2.0 SENSOR PLATFORM Organization: SAE/TP
Date: 2007-09-17
Description: These reconnaissance sensors are situated in a pod that is mounted to four arms to allow more than 200 degrees of rotation, and are mounted to a movable plate that allow for linear movement.
UFC 3-120-01 - AIR FORCE SIGN STANDARD Organization: UFC
Date: 2003-02-06
Description: Keep names of destinations consistent throughout the system, including the names on maps and the names used by security police when they are directing visitors to points on base. A direction sign pointing the way to the Personnel Center should lead to a building that is called the Personnel Center and not something else.
API PUBL 1132 - EFFECTS OF OXYGENATED FUELS AND REFORMULATED DIESEL FUELS ON ELASTOMERS AND POLYMERS IN PIPELINE/TERMINAL COMPONENTS Organization: API
Date: 1994-07-01
Description: Foundation bolts or fastenings l. Pedestal or base m. King post or Center Post RECORD RETENTION The manufacturer shall maintain all inspection and testing records for 20 years.
SAE AIR5662 - METHOD FOR PREDICTING LATERAL ATTENUATION OF AIRPLANE NOISE Organization: SAE
Date: 2006-04-01
Description: The methods for calculating the lateral attenuation of the sound apply to: turbofan-powered transport-category airplanes with engines mounted at the rear of the fuselage (on the sides of the fuselage or in the center of the fuselage as well as on the sides) or under the wings propeller-driven transport-category or general-aviation airplanes propagation over ground surfaces that may be considered to be "acoustically soft" such as lawn or field grass  situations where the terrain to the sides of the flight paths is not necessarily flat with receiver locations that are elevated above or depressed below the corresponding point on the ground under a flight path  flight paths that include turns such that the airplane is banked.
ASHRAE - OR-10-005 - HIGH DENSITY COOLING SOLUTIONS-TAKING IT TO THE NEXT LEVEL: THE COLD AISLE CONTAINMENT ALTERNATIVE Organization: ASHRAE
Date: 2010-01-01
Description: Even the revised ASHRAE specifications for operating conditions can increase heat removal capacity. But only up to a point. And at many locations, that point has been reached. With these greater loads and higher density installations becoming more commonplace, two newer methods are being deployed—aisle containment solutions and close-coupled heat transfer systems.

1 - 20 of 25 results