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LST power system long life design techniquesThe LST mission of up to 15 years plus about two years allotment for ground return maintenance could stretch the LST operation to the end of the century. This extended mission life, combined with the large power requirements of the telescope and the scientific instruments, imposes stringent requirements on the electrical power subsystem. The use of an onboard microprocessor for individual battery cell control and monitoring offers a technique that could improve the battery cycle life dramatically. The battery configuration includes spare battery cells which can be switched by the microprocessor to replace failed cells. The microprocessor can also be used for inflight reconditioning of the batteries to increase performance and verify ampere-hour capacity. The Flexible Roll-Up Solar Array (FRUSA) system offers a solar array at an acceptable cost that can stay within weight and volume constraints.
Document ID
19760029843
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, O. B.
(Martin Marietta Aerospace Denver, CO, United States)
Donovan, R. L.
(Martin Marietta Aerospace Denver, CO, United States)
Oberg, J. L.
(Martin Marietta Aerospace Denver, Colo., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AAS PAPER 75-182
Meeting Information
Meeting: Meeting on Space Shuttle Missions of the 80''s
Location: Denver, CO
Start Date: August 26, 1975
End Date: August 28, 1975
Sponsors: AAS, AIAA, IEEE, ORSA, and IMS,
Accession Number
76A12809
Funding Number(s)
CONTRACT_GRANT: NAS8-31312
Distribution Limits
Public
Copyright
Other

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