The SKYNET 4 constellation consists of three spacecraft which were launched between December 1988 and August 1990. The spacecraft are three-axis stabilized geostationary earth-orbiting military communications satellites with a design life of seven years on station. With the mission objective achieved all the batteries continue to give excellent performance. This paper presents a review of the history of the six batteries from cell procurement to the end of their design life and beyond. Differences in operational strategies are discussed and the lifetime trends in performance are analyzed. The combination of procurement acceptance criteria and the on-station battery management strategy utilized are presented as the prime factors in achieving...
Deployment of the American Satellite Company 1 spacecraft for the Space Shuttle Discovery in August ...
The handbook provides guidelines for the handling and storage of conventional NiCd flight batteries....
The interaction, effect, and controllability of the performance parameters of the General Electric 2...
Flight data for 17,000 orbital cycles are reviewed and summarized. The nickel cadmium battery system...
The Upper Atmosphere Research Satellite (UARS), designed, built, integrated, tested, and operated by...
The Earth Radiation Budget Satellite (ERBS), Compton Gamma Ray Observatory (CGRO), Upper Atmosphere ...
The advanced Television Infrared Observation satellite program is a cooperative effort between the N...
The US National Oceanic and Atmospheric Administration (NOAA) operates the Geostationary Operational...
The US National Oceanic and Atmospheric Administration (NOAA) operates the Polar Operational Environ...
The need for batteries with greater power capacity and service life for power satellites is examined...
The life durability of a nickel cadmium energy storage battery for the INTELSAT 5 Satellite is discu...
A life cycle test of secondary electric batteries for spacecraft applications was conducted. A sampl...
Results of testing, analysis, and development of lithium, nickel-cadmium, and nickel-hydrogen batter...
The in-flight performance data of two 17-cell, 6-ampere-hour nickel cadmium spacecraft batteries are...
NASA has developed battery technology to meet the demanding requirements for aerospace applications;...
Deployment of the American Satellite Company 1 spacecraft for the Space Shuttle Discovery in August ...
The handbook provides guidelines for the handling and storage of conventional NiCd flight batteries....
The interaction, effect, and controllability of the performance parameters of the General Electric 2...
Flight data for 17,000 orbital cycles are reviewed and summarized. The nickel cadmium battery system...
The Upper Atmosphere Research Satellite (UARS), designed, built, integrated, tested, and operated by...
The Earth Radiation Budget Satellite (ERBS), Compton Gamma Ray Observatory (CGRO), Upper Atmosphere ...
The advanced Television Infrared Observation satellite program is a cooperative effort between the N...
The US National Oceanic and Atmospheric Administration (NOAA) operates the Geostationary Operational...
The US National Oceanic and Atmospheric Administration (NOAA) operates the Polar Operational Environ...
The need for batteries with greater power capacity and service life for power satellites is examined...
The life durability of a nickel cadmium energy storage battery for the INTELSAT 5 Satellite is discu...
A life cycle test of secondary electric batteries for spacecraft applications was conducted. A sampl...
Results of testing, analysis, and development of lithium, nickel-cadmium, and nickel-hydrogen batter...
The in-flight performance data of two 17-cell, 6-ampere-hour nickel cadmium spacecraft batteries are...
NASA has developed battery technology to meet the demanding requirements for aerospace applications;...
Deployment of the American Satellite Company 1 spacecraft for the Space Shuttle Discovery in August ...
The handbook provides guidelines for the handling and storage of conventional NiCd flight batteries....
The interaction, effect, and controllability of the performance parameters of the General Electric 2...