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Title: Comparative energy storage assessment item

Technical Report ·
OSTI ID:5842674

This analysis, a Space Station application study, rediscovered Integrated Power and Attitude Control (IPAC) and found the approach to have lower initial and resupply weight and lower initial and resupply cost than either battery/CMG or regenerative fuel cell/CMG systems. Preliminary trade studies were performed comparing (IPAC) with equivalent independent electrochemical power and control moment gyro (CMG) control approaches. Technologies considered to have adequate status for an initial Space Station were: (1) nickel cadmium batteries (NiCd batteries), (2) regenerative fuel cells (RFC), (3) Skylab class CMG's, and (4) state of the art IPAC using metal wheels and ball bearing suspension (SOA-IPAC). An advanced IPAC (ADV-IPAC) employing composite rotor material and magnetic suspension was included in the comparisons to illustrate a possible range of performance and cost of inertial systems. The candidates were compared on the basis of initial weight and cost and on the basis of resupply weight and cost for a 15 year mission. Thus, SOA-IPAC would appear to be an attractive approach for the initial Space Station and possible technology improvements would further the appeal for the initial and/or growth Space Station.

Research Organization:
National Aeronautics and Space Administration, Huntsville, AL (USA). George C. Marshall Space Flight Center
OSTI ID:
5842674
Report Number(s):
N-85-13858
Resource Relation:
Other Information: In NASA, Langley Research Center, an assessment of integrated flywheel system technology, 91-99 p. (N--85-13850 05-20)
Country of Publication:
United States
Language:
English