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Energy Harvesting/Regeneration for Electric Vehicles Land, Water & Air 2015-2025

2014-12-01
The electric vehicle industry - land, water and air - is rapidly rising to become a market of over $533 billion by 2025. Some run entirely on harvested energy as with solar lake boats. Others recycle energy as with regenerative braking of cars, buses and military vehicles harvesting kinetic energy. Others use different forms of harvesting either to charge the traction batteries, or to drive autonomous device. In some cases, harvesting is making completely new forms of electric vehicle possible such as "glider" Autonomous Underwater Vehicles (AUVs) that can stay at sea for years, gaining electricity from both wave power and sunshine. Multiple forms of energy harvesting on one vehicle are becoming more common from cars to superyachts.
Standard

Fluid Couplings for Spacecraft Servicing, Preparation of Specification for, Metric

1993-06-09
CURRENT
MAP2261
This SAE Metric Aerospace Recommended Practice (MAP) establishes the requirements for preparing a specification for fluid couplings for spacecraft servicing. The objective of this document is to provide design, development, verification, storage, and delivery requirement guidelines for the preparation of specifications for fluid couplings and the ancillary hardware for use with serviceable spacecraft designed for use in the space environment. The couplings shall be capable of resupplying storable propellants, cryogenic liquids, and gases to a variety of spacecrafts.
SAE MOBILUS Subscription

Alternative Fuels

2015-02-11
This annual subscription delivers a comprehensive collection of more than 3,600 SAE technical papers, 60 standards, and 8 e-books covering a range of alternative fuels, including compressed natural gas, hydrogen fuel cells, and biodiesel. Content is updated regularly, so you’ll always have access to the latest research and thinking on this critical topic.
SAE MOBILUS Subscription

Wiley SAE MOBILUS® eBook Package

2018-03-23
Committed to being the primary source for aerospace and ground vehicle engineering resources, SAE International has added the full compilation of our Wiley eBook collections to the SAE MOBILUS® technical resource platform. Purchasable as an annual subscription and containing the titles from the Wiley Aerospace Collection, the Wiley Automotive Collection, the Wiley Computer Systems Collection, and the Wiley Cyber Security Collection.
Standard

TIN PLATING, IMMERSION

1991-10-01
HISTORICAL
AMS2409E
This specification covers the engineering requirements for producing a thin tin coating on aluminum alloys by an immersion process.
Standard

Plating, Brush, Tin-Zinc Low Hydrogen Embrittlement

2002-01-24
HISTORICAL
AMS2451/10
This specification covers the engineering requirements and process for brush plating of tin-zinc by electrodeposition. It is used, in conjunction with AMS 2451, for corrosion-protective, tin-zinc deposits, which may allow omission of hydrogen embrittlement relief treatment of high-strength steels.
Standard

Plating, Brush, Cobalt

2007-07-13
HISTORICAL
AMS2451/11A
This specification covers the requirements for brush plating of cobalt by electrodeposition.
Standard

Plating, Brush, Cobalt

2017-11-20
CURRENT
AMS2451/11B
This specification covers the requirements for brush plating of cobalt by electrodeposition.
Standard

Cryogenically Fueled Dynamic Power Systems

2011-08-03
CURRENT
AIR999A
In this report, "Cryogenically Fueled Dynamic Power Systems" include all open cycle, chemically fueled, dynamic engine power systems which utilize cryogenic fuels and oxidizers. For nearly all practical present day systems, this category is limited to cryogenic hydrogen or hydrogen-oxygen fueled cycles with potential in future, more advanced systems for replacement of oxygen by fluorine. Excluded from the category are static cryogenic systems (e.g., fuel cells) and chemical dynamic power systems which utilize earth storable propellants.
Standard

CRYOGENICALLY FUELED DYNAMIC POWER SYSTEMS

1968-10-01
HISTORICAL
AIR999
In this report, "Cryogenically Fueled Dynamic Power Systems" include all open cycle, chemically fueled, dynamic engine power systems which utilize cryogenic fuels and oxidizers. For nearly all practical present day systems, this category is limited to cryogenic hydrogen or hydrogen-oxygen fueled cycles with potential in future, more advanced systems for replacement of oxygen by fluorine. Excluded from the category are static cryogenic systems (e.g., fuel cells) and chemical dynamic power systems which utilize earth storable propellants.
Standard

Protective Breathing Equipment for Flight Deck and Cabin Crew Members

2002-08-19
CURRENT
AIR825/10A
This SAE Aerospace Information Report (AIR) provides general information to aircraft engineers, regarding the types of Protective Breathing Equipment (PBE) configurations which are available, the intended functions of such equipment, and the technical approaches which may be used in accomplishing these functions. The term "PBE" or "Protective Breathing Equipment" has been used to refer to various types of equipment, which are used in a variety of applications. This way of using the terminology has been a source of confusion in the aviation industry. One objective of this AIR is to assist the reader in distinguishing between the types of PBE applications. A further objective is to assist in understanding the technical approaches which can be used in each of the major applications. Principles of PBE design are reviewed briefly.
Standard

Protective Breathing Equipment for Flight Deck and Cabin Crew Members

2002-02-04
HISTORICAL
AIR825/10
This SAE Aerospace Information Report (AIR) provides general information to aircraft engineers, regarding the types of Protective Breathing Equipment (PBE) configurations which are available, the intended functions of such equipment, and the technical approaches which may be used in accomplishing these functions. The term "PBE" or "Protective Breathing Equipment" has been used to refer to various types of equipment, which are used in a variety of applications. This way of using the terminology has been a source of confusion in the aviation industry. One objective of this AIR is to assist the reader in distinguishing between the types of PBE applications. A further objective is to assist in understanding the technical approaches which can be used in each of the major applications. Principles of PBE design are reviewed briefly.
Standard

SAFE-LIFE LIMITS FOR LANDING GEAR STRUCTURES

2018-04-26
WIP
AIR6949
This document describes the approaches taken to define safe-life limits for the management of fatigue in landing gear structures, and the substantiation of those limits through full-scale fatigue testing. The safe-life scatter factors considered in a range of military and civil regulatory standards are also reviewed.
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