Introduction
Primary batteries are electrochemical devices that convert chemical energy into electrical energy and, unlike rechargeable batteries, are intended for single-use or “one shot” applications. They have a “niche” role in aerospace missions, especially where recharging is either not feasible or operationally difficult and/or where high specific energy density is desired. Planetary exploration missions are broadly categorized as orbiters, landers/rovers, probes, penetrators, and sample return capsules. While rechargeable batteries are exclusively the option for orbiters and small rovers; Probes, penetrators and sample return capsules are typically powered by primary batteries [1]. They are also used in launch vehicles to power pyro devices and on-board electronics guidance and control systems and in several miscellaneous applications, such as launch abort batteries and astronauts’ electronic devices, gadgets, and tools.
Primary batteries used in early spacecraft were largely of...
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References
Ratnakumar BV, Smart MC (2007) Aerospace applications – planetary exploration missions (orbiters, Landers, rovers and probes). In: Pistoia G, Broussely M (eds) Industrial applications of batteries. From electric vehicles to energy storage and toll collection. Elsevier, Amsterdam, pp 327–387
Dey AN (1977) Lithium anode film and organic and inorganic electrolyte batteries. Thin Solid Film 43:131
Serenyi R, Skelton J (2004) Proceedings of the 41st power sources conference, # 28.1, Philadelphia, 14 June 2004
Linden D, McDonald B (1980) The lithium—sulfur dioxide primary battery — its characteristics, performance and applications. J Power Sources 5:35, Elsevier Sequoia, Lausanne
Dagarin BP, Taenaka RK, Stofel EJ (1996) NASA battery workshop, p. 133
Ratnakumar BV, Smart MC, Kindler A, Frank H (2003) Potentiostatic depassivation of lithium-sulfur dioxide batteries on mars exploration rovers. J Power Sources 119:906
Ratnakumar BV, Smart MC, Ewell RC, Whitcanack LD, Kindler A, Narayanan SR, Surampudi S (2007) Potentiostatic depassivation of lithium-sulfur dioxide batteries on mars exploration rovers. J Electrochem Soc 154:A715–A724
Frank H, Deligiannis F, Davies E, Ratnakumar BV, Surampudi S, Russel PG, Reddy TB (1998) NASA battery workshop, Huntsville, 27 Oct 1998
Liang CC, Krehl PW, Danner DA, Appl J (1981) Bromine chloride as a cathode component in lithium inorganic cells. Electrochem 11:563–571
Whitacre J, Yazami R, Hamwic A, Smart MC, Bennett W, Surya Prakash GK, Miller T, Ratnakumar BV (2006) Low operational temperature Li–CFx batteries using cathodes containing sub-fluorinated graphitic materials. J Power Sources 160(1):577–584
Whitacre JF, West WC, Smart MC, Yazami R, Surya Prakash GK, Hamwi A, Ratnakumar BV (2007) Enhanced low-temperature performance of Li?–?CFx batteries. Electrochem Solid State Lett 10(7):A166–A170
West WC, Shevade A, Soler J, Kulleck J, Smart MC, Ratnakumar BV, Moran M, Haiges R, Christe KO, Surya Prakash GK (2010) Sulfuryl and thionyl halide-based ultralow temperature primary batteries. J Electrochem Soc 157:A571
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Bugga, R.V., Smart, M.C. (2014). Aerospace Applications for Primary Batteries. In: Kreysa, G., Ota, Ki., Savinell, R.F. (eds) Encyclopedia of Applied Electrochemistry. Springer, New York, NY. https://doi.org/10.1007/978-1-4419-6996-5_488
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