AbstractTo launching a spacecraft (rocket and satellite) including all of the systems, some rules and regulation of validation test for all the spacecraft systems is needed. Validation test mentioned is done to find out the ability of all the systems to the environmental influences of the external although internal with measurements simultaneously done. This is including possibilities the operating all of the electronic systems and epending the life times, operation time of the internal and external condition to the parameters effect of environmental the spacecraft systems. Thermal vibration is two parameters effect of environmental which would receiped simultaneously by the microsatellite or spacecraft on trajectory time when the spacecraf...
The launch phase is the most demanding mechanical environment typical satellites experience. In orde...
This article examines the new practice of Virtual Shaker Testing (VST), starting from its motivation...
In the frame of this thesis, novel vibration isolation systems for spaces launch vehicles are design...
This paper presents the basic research for establishing the qualification test (QT) level a unit has...
This paper presents the basic research for establishing the qualification test (QT) level which the ...
Since mid-2014, the fully integrated small satellite Flying Laptop is in the system testing phase at...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...
Most equipment are subjected to vibration environment during their useful life. It is seen that nea...
At the end of Space Shuttle mission, it re-enters the earth\u27s atmosphere with a speed that exceed...
This paper presents detailed flight-measured vibration data obtained during the five successful flig...
The satellite experiences the launch environment such as vibration, acceleration, shock induced by r...
OUFTI-1’s test campaigns were divided into two phases. The goal of Phase 1 is to demonstrate that th...
Rocket motor generates vibrations acting on whole rocket body including its contents. Part of the bo...
The results of a study into the environmental vibrations of a payload mounted on the Nike rocket lau...
Thorough thermal design and testing is compulsory for every satellite mission. A well-known thermal ...
The launch phase is the most demanding mechanical environment typical satellites experience. In orde...
This article examines the new practice of Virtual Shaker Testing (VST), starting from its motivation...
In the frame of this thesis, novel vibration isolation systems for spaces launch vehicles are design...
This paper presents the basic research for establishing the qualification test (QT) level a unit has...
This paper presents the basic research for establishing the qualification test (QT) level which the ...
Since mid-2014, the fully integrated small satellite Flying Laptop is in the system testing phase at...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...
Most equipment are subjected to vibration environment during their useful life. It is seen that nea...
At the end of Space Shuttle mission, it re-enters the earth\u27s atmosphere with a speed that exceed...
This paper presents detailed flight-measured vibration data obtained during the five successful flig...
The satellite experiences the launch environment such as vibration, acceleration, shock induced by r...
OUFTI-1’s test campaigns were divided into two phases. The goal of Phase 1 is to demonstrate that th...
Rocket motor generates vibrations acting on whole rocket body including its contents. Part of the bo...
The results of a study into the environmental vibrations of a payload mounted on the Nike rocket lau...
Thorough thermal design and testing is compulsory for every satellite mission. A well-known thermal ...
The launch phase is the most demanding mechanical environment typical satellites experience. In orde...
This article examines the new practice of Virtual Shaker Testing (VST), starting from its motivation...
In the frame of this thesis, novel vibration isolation systems for spaces launch vehicles are design...