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

Conference · Thu Jan 01 00:00:00 EST 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-
• Journal Information: Proc., Intersoc. Energy Convers. Eng. Conf.; (United States), Vol. 3; Conference: IECEC conference, Atlanta, GA, USA, 9 Aug 1981
• Country of Publication: United States
• Language: English

Related Subjects

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