Browse Topic: Tensile strength

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High performance unfilled polypropylene material for light weight interior trims2022-01-039303/29/2022
Light weighting is important to improve energy efficiency in the automotive industry. In this paper, high performance unfilled polypropylene copolymer (PPCP) material was selected and developed to reduce weight and cost without compromising on functional requirements for interior trims such as door trims, lower pillar trims, scuff trims and rear quarter trims (RQT). Interior trims are loaded with challenging requirements such as stiffness, dimensional stability, haptic feel, scratch resistance, cleanability, thermal stability, toughness, low emission and weathering resistance. Reactor polymerised PPCP material compound met these requirements by having ultra-flow behaviour, optimum tensile strength, balanced modulus - impact strength, scratch resistant, low emission and improved thermal properties. The combination of material, optimized part and tool design led to weight savings and considerable cost reduction.
Govindaraj, Karthik, Deoli, Manish, Gregory, Koch
Technical Paper
Ultra Flow, High Stiffness Polypropylene Material For Light Weight Exterior Trim Panels2022-01-039403/29/2022
Light weighting is an effective strategy in increasing energy efficiency in the automotive industry. In this paper, mass reduction with cost benefit was targeted in an exterior trim panel. Modified polypropylene copolymer (PPCP) material was developed for an exterior trim large panel (1400 X 700mm) with integrated grill mesh. The part had challenging requirements in terms of slow speed impact, structural durability, dimensional stability, aesthetics, thermal ageing resistance, cold impact resistance, scratch resistance and weathering resistance. The compounded PPCP material met these requirements by having ultra-flow behaviour, optimum tensile strength, modulus, impact strength and thermal properties. The combination of material, optimized part and tool design led to weight savings and considerable cost reduction.
Govindaraj, Karthik, Vimalathithan, Murukesan, YANAMANDRA, BHARADWAJA, D, VENKATESAN
Technical Paper
Development of 1520 MPa Class Lightweight Suspension Springs2022-32-002401/09/2022
The spring is an important component part of the suspension of motorcycles and automobiles. As the spring constitutes an unsprung weight, the suspension complies more quickly if the spring weighs less. Especially in off-road motorcycles, which are often subjected to extremely hard conditions such as full acceleration and braking, quick turning and jumping, a reduction of unsprung weight contributes to an enhancement of dynamic performance. As an effective means to reduce weight, use of the light-weight titanium instead of the commonly used steel is seen in some examples. However, applications of titanium are limited only to large-diameter springs because of its higher cost and challenging in coiling. To achieve a steel spring that weighs lower than a titanium counterpart, we aimed at a spring that features such a fatigue strength that allows stressing as higher as to 1520 MPa. Three technical options are used, 1) Shot peening, 2) Removal of decarburized surface on wire material, 3
Kato, Hideki, Kasatori, Shinji, Kameda, Hirokatsu, Suzuki, Shoichi
Technical Paper
Steel, Bars, Forgings, Mechanical Tubing and Forging Stock 0.50Cr - 0.12Mo (0.89 - 1.01C)AMS6476F-TEST-REC (Historical)11/09/2021
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging or tubing stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel, Bars, Forgings, Mechanical Tubing and Forging Stock 0.50Cr - 0.12Mo (0.89 - 1.01C)AMS6476F (Current)11/09/2021
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging or tubing stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel, Bars, Forgings, and Tubing 1.2Cr - 2.0Ni - 0.45Mo (0.27 - 0.33C)AMS6407L-TEST-REC (Historical)10/22/2021
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Low-Alloy Steel, Heat-Resistant, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.95Cr - 0.55Mo - 0.30V (0.40 - 0.50C)AMS6304N-TEST-REC (Historical)10/22/2021
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel, Bars, Forgings, Mechanical Tubing and Forging Stock 1.2Cr - 3.25Ni - 0.12Mo (0.07 - 0.13C) (9310) Vacuum Consumable Electrode RemeltedAMS6265R (Current)10/22/2021
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Low-Alloy Steel, Heat-Resistant, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.95Cr - 0.55Mo - 0.30V (0.40 - 0.50C)AMS6304N (Current)10/22/2021
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel, Bars, Forgings, and Tubing 1.2Cr - 2.0Ni - 0.45Mo (0.27 - 0.33C)AMS6407L (Current)10/22/2021
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel Bars, Forgings, and Mechanical Tubing and Forging Stock 1.2Cr - 3.25Ni - 0.12Mo (0.07 - 0.13C) (9310) Electroslag Remelted or Consumable Electrode Vacuum RemeltedAMS6267K (Current)10/22/2021
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Insulating Component, Molded, Electrical, Heat Shrinkable, Connector and Cable Accessory, Sealing Strain Relief, General Specification ForAS5258A-TEST-REC (Historical)10/13/2021
This specification covers connector and cable accessory heat shrinkable, electrical insulating, molded components fabricated from various polymer based compositions. These components are intended for use as connector and cable accessory components to provide strain relief, electrical insulation, and environmental sealing.
AE-8C1 Connectors Committee
Technical Standard
Insulating Component, Molded, Electrical, Heat Shrinkable, Connector and Cable Accessory, Sealing Strain Relief, General Specification ForAS5258A (Current)10/13/2021
This specification covers connector and cable accessory heat shrinkable, electrical insulating, molded components fabricated from various polymer based compositions. These components are intended for use as connector and cable accessory components to provide strain relief, electrical insulation, and environmental sealing.
AE-8C1 Connectors Committee
Technical Standard
Mechanical property optimization of tamarind fruit fiber for lightweight structural composites applications2021-28-027010/01/2021
Natural fibers are dominating many composite industries due to their unique properties such as reusability, biodegradability, and environmental safety. Tamarind fruit fiber (TFF) stands out among the various fruit fibers and has been discovered in large quantities being discarded from the food processing industries. However, many natural fibers are extracted from their sources, which results in deforestation and environmental degradation. As a result, in today's world, recycling waste into new useful products is the primary concern in any field of engineering. In light of this, the current study used TFF obtained from agro industries and processed into fibers, which were then mixed with an unsaturated polyester matrix to create a natural composite material. Furthermore, by considering process parameters and their levels for conducting experiments, an orthogonal array has been achieved using Taguchi's design approach. The effect of different fiber diameters in relation to various gauge
Joseph Selvi, Binoj, Natarajan PhD, Manikandan, Pattipati Chinna PhD, Krishnamachary, Karu Clement PhD, Varaprasad, Pasupuleti, Thejasree, Justin Abraham Baby PhD, Sajin
Technical Paper
Impact of Post Processing Methods on the Mechanical Properties of Squeeze Casted A356 Alloy2021-28-026610/01/2021
This research is contracted to study the impact of post processing routes like heat treatment and heat treated cum shot peening approach on the mechanical characteristics of A356 alloy. A356 alloy composed of aluminium, silicon, magnesium, iron and copper act as a most promising aluminium alloy due to its phenomenal cast ability, corrosion resistant and great strength to weight proportion. A356 is a common industrial alloy due to its great mechanical properties, reduced weight and capability to be casted into complex designs. However, in order to display good static mechanical properties, it must be heat treated. The prime objective of this research work is to compare the mechanical attributes of squeeze casted pure A356 alloy with the samples processed through T6 heat treatment and heat treatment cum shot peening approach. Mechanical responses like hardness, tensile strength and impact strength were measured for the fabricated post processed samples. There is a noteworthy improvement
A, Sathishkumar, R, Soundararajan, Kalidasan, Reshvanth, Ganapathy, Sakthivel
Technical Paper
Microstructural changes and Mechanical properties upgrading over Friction Stir Processing strategies on A356 alloy with tungsten nano particle surface layer composites2021-28-026910/01/2021
Friction stir processing (FSP) is a typical process for refinement changes of microstructure, upgradation of material’s mechanical properties and fabricating of surface layer composites. The effect of cast A356 surface composites were fabricated through Friction Stir Processing (FSP) route to appraise the metallurgical and mechanical properties were considered in the present research study. The three combination of test samples of FSP’ed cast A356 alloy, FSP’ed cast A356 FSP with tungsten nano particle addition (5 and 10 vol%) were considered to fabrication under fixed parametric conditions like tool rotational speed of 1000 rpm, load acting 9 kN, tool travel speed of 20 mm min−1 through four number of tool travel passes respectively. Obtained FSP’ed samples were exposed to microstructural, tensile strength tests and fracture surface morphology analysis were carried out to record the responses. It was observed in stir zone microstructure that the FSP parameters have affected the
R, Soundararajan, Prince Edward, Jerald Immanuel, Venkitkumar, Nishanth, Aruchamy, Sathishkumar
Technical Paper
An experimental investigation on hot cracking and properties of TIG welded AA2014 alloy using continuous current and pulsed current2021-28-026210/01/2021
AA2014 Aluminum alloys are most widely used for automobile and aerospace structures where specific strength is important. Hot cracking is a major problem while welding these alloys. In the present investigation, the metallurgical studies, viz, hot cracking sensitivity, microstructure and the mechanical properties, viz, hardness and tensile strength of the 4 mm thickness AA2014 aluminum alloy were studied using two different methods. The first method involves TIG (Tungsten Inert Gas) welding with continuous current process and the second method involves TIG welding with pulsed current process. In the both the process commercial argon pure gas was used as a shielding gas. The results showed that hot cracking sensitivity was decreased when the specimen was welded using pulsed current process compared to continuous current process. Similarly, the specimen was welded with pulsed current process showed improved mechanical properties compared to continuous current process because of low heat
Kaliyaperumal, Balasubramanian, R, Soundararajan, Rengaraj, Jeyakumar, Rangasamy, Ramamoorthi
Technical Paper
Experimental Modal Analysis Study on Graphene filled SBR2021-28-022510/01/2021
Rubbers are widely used in many engineering applications such as tubes, timing belt, tyre etc. Apart from its functional use, it can also be used as damping material in many applications in order to dampen the vibrations transmitted from one structure to other. The present research work focus on the development of CB filled SBR and Graphene filled SBR. Both rubber samples were investigated for its mechanical properties such as hardness and tensile strength. Experimental modal analysis was also done to examine the dynamic characteristics such as damping and natural frequency along with its mode shapes for the prepared samples and compared. It is observed from the results that the inclusion of graphene in SBR improved its vibration characteristics in addition to the improvement of mechanical properties.
Natarajan, Ravikumar, S, Rizwan Asif, C, Sivakumar, Manohar, D Murali
Technical Paper
Mechanical and microstructural behaviour of friction stir welded Al6061/Cr2O3 metal matrix composite.2021-28-022410/01/2021
Aluminium metal matrix composite are widely used in various field like aerospace, marine and automobile application. The application of composites necessitates joining process and its difficult due to different materials. To address the considering difficulties the present study is, Cr2O3 was reinforced in Al 6061 matrix in 2% to 6% in the incremental step of 2%. The stir casting technique was used to fabricate the composites with 300rpm stirring speed and the stirring time duration was 3min throughout the fabrication process. The PCBN tool is used for prepared friction stir welded (FSW) joints and tool having 6.7mm pin diameter and 6mm pin height. The fabrication process is conducted by 1000rpm tool rotational speed and 25mm/min welding speed. The atmospheric and underwater environmental conditions was preferred to perform friction stir welding. The mechanical properties of the joint, such as tensile strength (ASTM E8), hardness (ASTM E18) and impact strength (ASTM E23) are
K, Senthilraj, Govindasamy, Rajamurugan, Krishnasamy, Prabu, Uday, KN
Technical Paper
Test Slabs, Chloroprene (CR) 70 - 80AMS3217/3D (Current)10/01/2021
This specification covers a standard chloroprene (CR) rubber stock in the form of molded test slabs.
AMS CE Elastomers Committee
Material Specification
Inspection and Test Quality Systems, Requirements for Aviation, Space, and Defense OrganizationsAS9003B09/30/2021
Price increases in effect for this document as of January 2017 reflect a new copyright agreement for use of ISO 9001:2009. This standard includes selected quality system requirements from ISO 9001:2008[1] and AS9100:2009 applicable to noncomplex products and associated manufacturing processes. ISO 9001 text incorporated into this standard appears in standard font; while aviation, space, and defense industry additional requirements, definitions, and notes are presented in bold, italic text. The requirements of this standard are intended to be applied in whole, without any exclusions. Compliance with all corresponding AS9100 requirements is considered to meet/exceed compliance with the requirements of this standard. The requirements specified in this standard are complementary (not alternative) to contractual and applicable statutory and regulatory requirements. Should there be a conflict between the requirements of this standard and applicable statutory or regulatory requirements, the
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Technical Paper
citation check in edgeSAE-PP-0046309/29/2021
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SintzADMIN, Jeneane, SintzUSER, Jeneane
Pre-Print Article
A Case study on Effect of subsequent operations on shotpeened Crown Wheel Pinion (Hypoid Gear set) & Compressive Residual Stress analysis2021-26-025209/22/2021
Abstract: The prime function of crown wheel pinion is to receive the power from Transmission & distribute to two-wheel Ends. Doing so these members will experience the tremendous Bending Fatigue. Shot peen is the one of the latest technologiesused to improve the bending Fatigue of the CWP. In this particular case- 6 CWP are taken for the Study to understand the effect of the operations after shot peen process. 3 Samples are named as Batch A, another 3 samples are named as Batch B. Both the batch CWP are shot peened. Then as a regular production Practice the Batch A CWP are process through Hard TurningAbrasive Lapping Hot Lubriting (Mn Phosphate)Fully Finish Ready for Assembly. Then Both the Batch A & batch B samples are taken for Residual Stress analysis using X-Ray Diffraction Technique. The measurement location is 50 microns below the surface. The results tabulated,found that Batch A samples shows decrease in Residual stress relatively to Batch B.This evident that post operations
Rao, Yathish
Technical Paper
Effect of Welding Consumables on Static and Dynamic Properties of Representative Welded Joints for Chassis Structure2021-26-025909/22/2021
Automotive suspension system forms the basis for the design of vehicle with durability, reliability and NVH requirements. The automotive suspension systems are exposed to dynamic and static loads which in turn demands the highest integrity and performance against fatigue based metallic degradation. The current focus in automotive industry is to reduce the weight of the automotive parts and components without compromising with its static and dynamic mechanical properties. This weight reduction imparts fuel efficiency with added advantages. High-strength low alloy steel (HSLA) offers optimum combination of mechanical properties. Furthermore, welding processes offer design flexibility to achieve robust and lightweight designs with high strength steels. However, welding process has to be established to get optimum benefits of high strength steels with minimal adverse effects and deterioration of the static and dynamic mechanical properties of the weldments. In current work, effect of
Chauhan, Shiv, Varatharajan, Senthilkumaran, Shende, Deodatta
Technical Paper
Experimental investigations on material compatibility of a methanol fuel supply system of a spark ignition engine2021-01-118909/21/2021
Material compatibility of fuel supply system comprised of different materials including elastomers (nitrile, polyvinyl chloride (PVC) nitrile, chloroprene, natural rubber and ethylene-propylene-diene monomer (EPDM)), aluminium and fuel filter (outer tin coated circular plate and paper) with methanol was studied. The specimens of the parts of the fuel supply system were immersed in methanol for a period of ninety days under atmospheric conditions. The properties of the specimens such as physical changes using scanning electron microscope (SEM) image of the surfaces and mechanical properties including tensile strength and strain at break were studied. It was observed from the images that the coating over the circular plate of fuel filter eroded while elastomers developed a whitish coat on their surfaces. SEM images indicated surfaces of EPDM, chloroprene and natural rubber were damaged significantly. Diffusion of methanol inside the elastomers negatively impacted on the increased mass of
Nidhi, Nidhi, Subramanian, K.A.
Technical Paper
WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, NORMAL WEIGHT, 80 MICROINCH SILVER-COATED HIGH-STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHSAS22759/49B (Current)09/20/2021
AE-8D Wire and Cable Committee
Technical Standard
T-Bolt and Eye Bolt, A286 CRES, 1000 °F Fatigue RatedAS4108D (Current)09/01/2021
This specification defines the requirements for A286 CRES T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Technical Standard
BOLT, MACHINE - DOUBLE HEX HEAD, REDUCED SHANK, UNS N07718 - 185 KSIAS3650B (Historical)09/01/2021
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
BOLT, MACHINE - DOUBLE HEX HEAD, REDUCED SHANK, UNS N07718 - 185 KSIAS3650B-TEST-REC (Historical)09/01/2021
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
T-Bolt and Eye Bolt, A286 CRES, 1000 °F Fatigue RatedAS4108D-TEST-REC (Historical)09/01/2021
This specification defines the requirements for A286 CRES T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Technical Standard
Steel Bars, Forgings, and Mechanical Tubing and Forging Stock 1.1Si - 1.45Cr - 1.0Mo - 0.08Al (0.16 - 0.22C) Double Vacuum MeltedAMS6255G (Current)08/26/2021
This specification covers a premium aircraft quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
CONTACTS, ELECTRICAL CONNECTORS, PIN, SOLDER, REMOVABLE, SHIELDED, SIZE 12 (FOR MIL-DTL-83723 SERIES III CONNECTORS)AS39029/74C (Current)08/23/2021
AE-8C1 Connectors Committee
Technical Standard
Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)AMS2759/1J (Current)08/03/2021
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of carbon and low-alloy steel parts to minimum ultimate tensile strengths below 220 ksi (1517 MPa). Parts are defined in AMS2759. Due to limited hardenability in these materials, there are size limits in this specification.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, 90 DEGREE, SELF LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMODATION, CATEGORY 3B FOR MIL-DTL-38999 SERIES III AND IV CONNECTORSAS85049/117D (Current)07/30/2021
AE-8C1 Connectors Committee
Technical Standard
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, STRAIGHT, NON-SELF LOCKING AND SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-83723 SERIES III, AS50151 CRIMP, AS95234, AS81703 SERIES III, AND MIL-DTL-26482 SERIES II CONNECTORS)AS85049/109D (Current)07/30/2021
AE-8C1 Connectors Committee
Technical Standard
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS)AS39029/84B (Current)07/30/2021
AE-8C1 Connectors Committee
Technical Standard
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, 90 DEGREE, SELF-LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)AS85049/114D (Current)07/30/2021
AE-8C1 Connectors Committee
Technical Standard
Fusion Splice for Aerospace Fiber Optic CablesAS6506/1 (Current)07/23/2021
This specification includes detailed requirements for a fiber optic cable splice compliant with AS6506. Every requirement of the parent standard, AS6506, which applies to this detail specification is identified below by the word “applicable.” In any case in which a requirement of this specification varies from that of the parent standard, the alternate requirement is described. If a parent standard requirement does not apply, the words used are “not applicable.”
AS-3 Fiber Optics and Applied Photonics Committee
Technical Standard
Steel, Bars, Forgings, and Mechanical Tubing 0.50Cr - 0.55Ni - 0.20Mo (0.18 - 0.23C) (SAE 8620)AMS6274S (Current)07/23/2021
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
CABLE, LOW INDUCTANCE, 270 VOLT DCAS5756/7B (Current)07/15/2021
AE-8D Wire and Cable Committee
Technical Standard
Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally AgedAMS4146H-TEST-REC (Historical)07/07/2021
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Material Specification
Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and HigherAMS2759/2K (Current)07/07/2021
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of low-alloy steel parts to minimum ultimate tensile strengths of 220 ksi (1517 MPa) and higher. Parts are defined in AMS2759. The requirements for heat treatment of alloy Aermet100 are no longer part of this specification and can be found in AMS2759/3. Due to the limited hardenability of these materials, size limits have been added to this specification.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally AgedAMS4146H (Current)07/07/2021
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Material Specification
CABLE, ELECTRIC, FILTER LINE, SHIELDED, JACKETED, RADIO FREQUENCY ABSORPTIVE, 150 °C, 600-VOLTAS85485/8B (Current)06/22/2021
AE-8D Wire and Cable Committee
Technical Standard
CABLE, ELECTRIC, FILTER LINE, SMALL DIAMETER WIRE, SHIELDED, JACKETED, RADIO FREQUENCY ABSORPTIVE, 150 °C, 600-VOLTAS85485/12B (Current)06/22/2021
AE-8D Wire and Cable Committee
Technical Standard
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, STRAIGHT, SELF LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)AS85049/115D (Current)06/22/2021
AE-8C1 Connectors Committee
Technical Standard
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, STRAIGHT, SELF LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)AS85049/112D (Current)06/22/2021
AE-8C1 Connectors Committee
Technical Standard
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, 90 DEGREE, SELF LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-83723 SERIES III, AS50151 CRIMP, AS95234, AS81703 SERIES III, AND MIL-DTL-26482 SERIES II CONNECTORS)AS85049/111D (Current)06/22/2021
AE-8C1 Connectors Committee
Technical Standard
CONTACTS, ELECTRICAL CONNECTORS, SOCKET, SOLDER, REMOVABLE, SHIELDED, SIZE 12 (FOR MIL-DTL-83723 SERIES III CONNECTORS)AS39029/73C (Current)06/10/2021
AE-8C1 Connectors Committee
Technical Standard
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSS-LINKED MODIFIED ETFE, NORMAL WEIGHT, NICKEL-COATED, HIGH STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHSAS22759/42A (Current)06/07/2021
AE-8D Wire and Cable Committee
Technical Standard
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