In-flight performance of the solar maximum mission electrical power system

Conference · Thu Jan 01 04:00:00 UTC 1981 · Proc., Intersoc. Energy Convers. Eng. Conf.; (United States)

OSTI ID:5354661

Broderick, R J

The Solar Maximum Mission (SMM) is the first satellite to use the Multimission Modular Spacecraft (MMS) base module. The Modular Power Subsystem (MPS) is one of the major subsystems of the MMS. The in-flight performance of the MPS and the other components of the Electrical Power System (EPS) for the first 18 months of the mission is discussed. Details of performance such as solar array current and voltage degradation, Standard Power Regulator Unit (SPRU) efficiency, peak power tracking accuracy, battery charge to discharge ratio, battery voltage degradation and battery differential voltage characteristics are discussed.

• Research Organization: NASA, Goddard Space Flight Cent, Greenbelt, Md, USA
• OSTI ID: 5354661
• Report Number(s): CONF-810812-
• Conference Information: Journal Name: Proc., Intersoc. Energy Convers. Eng. Conf.; (United States) Journal Volume: 3
• Country of Publication: United States
• Language: English

Related Subjects

14 SOLAR ENERGY
140600* -- Solar Energy-- Photovoltaic Power Systems
ELECTRIC BATTERIES
ELECTROCHEMICAL CELLS
ELECTRONIC EQUIPMENT
EQUIPMENT
PERFORMANCE
POWER SUPPLIES
SOLAR CELL ARRAYS
SOLAR EQUIPMENT
SPACECRAFT POWER SUPPLIES