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Author: National Aeronautics and Space Administration (NASA) Publisher: Createspace Independent Publishing Platform ISBN: 9781720656746 Category : Languages : en Pages : 44
Book Description
This document provides an overview of the design, development, and application of nickel-hydrogen (Ni-H2) battery technology for aerospace applications. It complements and updates the information presented in NASA RP-1314, NASA Handbook for Nickel- Hydrogen Batteries, published in 1993. Since that time, nickel-hydrogen batteries have become widely accepted for aerospace energy storage requirements and much more has been learned. The intent of this document is to capture some of that additional knowledge. This document addresses various aspects of nickel-hydrogen technology including the electrochemical reactions, cell component design, and selection considerations; overall cell and battery design considerations; charge control considerations; and manufacturing issues that have surfaced over the years that nickel-hydrogen battery technology has been the major energy storage technology for geosynchronous and low-Earth-orbiting satellites.Thaller, Lawrence H. and Zimmerman, Albert H.Glenn Research CenterNICKEL HYDROGEN BATTERIES; HYDROGEN; MANUFACTURING; TECHNOLOGY UTILIZATION; DESIGN ANALYSIS; ELECTRIC BATTERIES; EARTH ORBITS; AEROSPACE ENGINEERING; ENERGY STORAGE; HANDBOOKS
Author: National Aeronautics and Space Administration (NASA) Publisher: Createspace Independent Publishing Platform ISBN: 9781720656746 Category : Languages : en Pages : 44
Book Description
This document provides an overview of the design, development, and application of nickel-hydrogen (Ni-H2) battery technology for aerospace applications. It complements and updates the information presented in NASA RP-1314, NASA Handbook for Nickel- Hydrogen Batteries, published in 1993. Since that time, nickel-hydrogen batteries have become widely accepted for aerospace energy storage requirements and much more has been learned. The intent of this document is to capture some of that additional knowledge. This document addresses various aspects of nickel-hydrogen technology including the electrochemical reactions, cell component design, and selection considerations; overall cell and battery design considerations; charge control considerations; and manufacturing issues that have surfaced over the years that nickel-hydrogen battery technology has been the major energy storage technology for geosynchronous and low-Earth-orbiting satellites.Thaller, Lawrence H. and Zimmerman, Albert H.Glenn Research CenterNICKEL HYDROGEN BATTERIES; HYDROGEN; MANUFACTURING; TECHNOLOGY UTILIZATION; DESIGN ANALYSIS; ELECTRIC BATTERIES; EARTH ORBITS; AEROSPACE ENGINEERING; ENERGY STORAGE; HANDBOOKS
Author: National Aeronautics and Space Administration (NASA) Publisher: Createspace Independent Publishing Platform ISBN: 9781725040267 Category : Languages : en Pages : 30
Book Description
This paper on nickel hydrogen batteries is an overview of the various nickel hydrogen battery design options, technical accomplishments, validation test results and trends. There is more than one nickel hydrogen battery design, each having its advantage for specific applications. The major battery designs are individual pressure vessel (IPV), common pressure vessel (CPV), bipolar and low pressure metal hydride. State-of-the-art (SOA) nickel hydrogen batteries are replacing nickel cadmium batteries in almost all geosynchronous orbit (GEO) applications requiring power above 1 kW. However, for the more severe low earth orbit (LEO) applications (greater than 30,000 cycles), the current cycle life of 4000 to 10,000 cycles at 60 percent DOD should be improved. A NASA Lewis Research Center innovative advanced design IPV nickel hydrogen cell led to a breakthrough in cycle life enabling LEO applications at deep depths of discharge (DOD). A trend for some future satellites is to increase the power level to greater than 6 kW. Another trend is to decrease the power to less than 1 kW for small low cost satellites. Hence, the challenge is to reduce battery mass, volume and cost. A key is to develop a light weight nickel electrode and alternate battery designs. A common pressure vessel (CPV) nickel hydrogen battery is emerging as a viable alternative to the IPV design. It has the advantage of reduced mass, volume and manufacturing costs. A 10 Ah CPV battery has successfully provided power on the relatively short lived Clementine Spacecraft. A bipolar nickel hydrogen battery design has been demonstrated (15,000 LEO cycles, 40 percent DOD). The advantage is also a significant reduction in volume, a modest reduction in mass, and like most bipolar designs, features a high pulse power capability. A low pressure aerospace nickel metal hydride battery cell has been developed and is on the market. It is a prismatic design which has the advantage of a significant reduction in volume and a ...
Author: Albert H. Zimmerman Publisher: Aerospace Corporation ISBN: 9781884989209 Category : Technology & Engineering Languages : en Pages : 495
Book Description
Nickel-hydrogen battery cells provide one of the longest-lived and most reliable rechargeable battery systems ever developed. The Aerospace Corporation was instrumental in the research, development, and testing of such batteries. Primarily developed for use in satellite and space power systems, their exceptionally long life was well worth the high cost associated with the technology, and they rapidly replaced most of the nickel-cadmium batteries used in earlier satellites. This book provides the reader with an in-depth view of nickel-hydrogen cell technology: how it was developed, how and why it works, how to implement it and realize its ultimate capability, and what can go wrong if it is not properly managed.
Author: Lawrence H. Thaller Publisher: AIAA ISBN: 9781884989131 Category : Technology & Engineering Languages : en Pages : 212
Book Description
The review and analysis reported here are the outcomes of a project carried out from 1998-2001 within the Energy Technology Department of the The Aerospace Corporation to examine the available results of different nickel-hydrogen life testing programs that had been or were being carried out for low Earth orbit (LEO) applications. The cycling programs, some of which are still in progress, were conducted under different sponsorships and carried out at different testing facilities.
Author: National Aeronautics and Space Administration (NASA)
Author: National Aeronautics and Space Administration (NASA)
Author: United States. National Aeronautics and Space Administration
Author: Lawrence H. Thaller
Author: James D. Dunlop
Author: National Aeronautics and Space Administration (NASA)
Author: 
Author: Albert H. Zimmerman
Author: 
Author: Lawrence H. Thaller
Author: John E. Clifford