As the satellite system becomes more complex, the probability of unpredictable failures may be increased due to design inadequacy, experience deficiency, lack of problem recognition. Poor quality control, improper testing, and workmanship fault. Consequently, these problems can lead to the reduction or end of the satellite mission lifetime. This article addresses general satellite failure modes and factors influencing satellite mission life. The mission life factors of LEO sun-synchronous KOMPSAT spacecraft are investigated, in which its mission life is predicted based on these factors. Since the end of mission due to random failures is not predictable, the predictable mission life factors such as power budget, propellant budget, battery ch...
A satellite power system should generate and supply sufficient electric power to perform the satelli...
In this paper, KOMPSAT satellite launch and deployment operations are discussed. The U.S. Taurus lau...
Maneuvers require velocity augmentation to control a satellite at the defined orbit. The velocity au...
Estimating the operational lifetime of satellites and spacecraft is a complex process. Operational l...
Following a business as usual scenario, some Low Earth Orbit (LEO) regions could be unusable for man...
The satellite technology has been attracting the attention of governments and companies with increas...
This paper addresses research completed for predicting hardware failures and estimating remaining du...
Spacecraft payloads are the sensing components that remain active over time and ensure Spacecraft's ...
Advances in the small satellite combined with the availability of low-cost launches have led to an i...
International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and...
This paper presents a satellite failure analysis for Low Earth Orbit (LEO) constellations with conti...
The estimation of the operational lifetime of a satellite is a challenging task, difficult to genera...
Spacecraft fulfill a myriad of critical functions on orbit, from defense and intelligence to science...
For satellites in Geostationary Earth Orbit (GEO) the available propellant mass leads to a limited y...
Due to factors relating to normal satellite degradation or unexpected anomalous conditions, a satell...
A satellite power system should generate and supply sufficient electric power to perform the satelli...
In this paper, KOMPSAT satellite launch and deployment operations are discussed. The U.S. Taurus lau...
Maneuvers require velocity augmentation to control a satellite at the defined orbit. The velocity au...
Estimating the operational lifetime of satellites and spacecraft is a complex process. Operational l...
Following a business as usual scenario, some Low Earth Orbit (LEO) regions could be unusable for man...
The satellite technology has been attracting the attention of governments and companies with increas...
This paper addresses research completed for predicting hardware failures and estimating remaining du...
Spacecraft payloads are the sensing components that remain active over time and ensure Spacecraft's ...
Advances in the small satellite combined with the availability of low-cost launches have led to an i...
International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and...
This paper presents a satellite failure analysis for Low Earth Orbit (LEO) constellations with conti...
The estimation of the operational lifetime of a satellite is a challenging task, difficult to genera...
Spacecraft fulfill a myriad of critical functions on orbit, from defense and intelligence to science...
For satellites in Geostationary Earth Orbit (GEO) the available propellant mass leads to a limited y...
Due to factors relating to normal satellite degradation or unexpected anomalous conditions, a satell...
A satellite power system should generate and supply sufficient electric power to perform the satelli...
In this paper, KOMPSAT satellite launch and deployment operations are discussed. The U.S. Taurus lau...
Maneuvers require velocity augmentation to control a satellite at the defined orbit. The velocity au...