Home  |   Login  |   Logout  |   Access Information  |   Alerts  |   Purchase History  |   Cart  |   Sitemap  |   Help   
 
Abstract
BROWSE SEARCH IEEE XPLORE GUIDE SUPPORT
arrow_leftView TOC
Email/Printer Friendly Format  
 

Lithium-ion batteries for aerospace
Smart, M.C.   Ratnakumar, B.V.   Whitcanack, L.D.   Chin, K.B.   Surampudi, S.   Gitzendanner, R.   Puglia, F.   Byers, J.  
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA;

This paper appears in: Aerospace and Electronic Systems Magazine, IEEE
Publication Date: Jan 2004
Volume: 19,  Issue: 1, Part 1
On page(s): 18- 25
ISSN: 0885-8985
INSPEC Accession Number: 8018133
Digital Object Identifier: 10.1109/MAES.2004.1263988
Current Version Published: 2004-08-16

Abstract
Under the Mars Surveyor Program (MSP01), lithium-ion batteries were developed by Lithion Inc. (Yardney Technical Products Inc.), each being 28 V, 25 Ah, 8-cells, 9 kg and fully qualified prior to mission cancellation. In addition to the requirement of being able to supply at least 90 cycles on the surface of Mars, the battery was demonstrated to be capable of operation (both charge and discharge) over a large temperature range (-20° to +40°C), with tolerance to non-operational excursions to -30° and +50°C. After mission cancellation, the batteries delivered to JPL were subjected to generic performance tests to demonstrate the applicability of the technology to meet future NASA aerospace applications. One of the two batteries currently being tested at JPL is undergoing testing according to anticipated performance requirements of future Mars Lander applications. The primary goal of this activity is to determine the performance capability to power surface operation on Mars for a prolonged period (> 3 years) after being subjected to a long cruise period. The second 25 AHr battery is being tested to determine the viability of using lithium-ion technology for future planetary orbiter applications. The test implemented consists of cycling the battery continuously under LEO conditions (30% DOD), while periodically checking the battery impedance and full capacity (100% DOD). Prior to initiating these tests, a number of characterization tests were performed to determine general performance attributes and battery health. In addition to presenting battery data, results obtained with individual cells will also be presented to further describe the capabilities of the technology to meet future applications.

Index Terms
Available to subscribers and IEEE members.

References
Available to subscribers and IEEE members.
Citing Documents
Available to subscribers and IEEE members.
You are not logged in.
Guests may access Abstract records free of charge.
Login
Username
Password
» Forgot your password?
Please remember to log out when you have finished your session.
You must log in to access:
• Advanced or Author Search
• CrossRef Search
• AbstractPlus Records
• Full Text PDF
• Full Text HTML
Access this document
Full Text: PDF (908 KB)
» Buy this document now
»  Learn more about
»  Learn more about
    purchasing articles
    and standards

Rights and Permissions
» Learn More
Download this citation
Available to subscribers and IEEE members.
 
arrow_leftView TOC   |  Back to toparrow_up
Indexed by IEE Inspec
© Copyright 2009 IEEE – All Rights Reserved