NORSAT-1 is a multi-payload microsatellite mission funded by the Norwegian Space Center, with three overall objectives: investigating solar radiation, space plasma research, and developing improved methods for detection and management of ship traffic. The successful development of the NORSAT-1 platform aims to lay the groundwork for additional low-cost microsatellites in the NORSAT series, and expand the Norwegian presence in space and space-based ship tracking technologies. This thesis provides some insight into the NORSAT-1 satellite platform design, and focuses heavily on the mechanical aspects of design, analysis, and testing. The structural design is detailed from the early conceptual design phases, and follows the development to the m...
Low-cost microsatellites structures represent an extremely interesting challenge and a excellent tec...
[[abstract]]One of the main advantage of microsatellites is their small size. The reliability, safet...
Mass reduction is a primary design goal pursued in satellite structural design, since the launch cos...
NORSAT-1 is a multi-payload microsatellite mission funded by the Norwegian Space Center, with three ...
NORSAT-2 is a 16-kilogram microsatellite designed, constructed and tested at the University of Toron...
There is an increasing need for monitoring and regulation of maritime vessels. This regulation can h...
The rapid development of small satellite technologies and the lowering cost of launch services have ...
An evolution is undergoing in the satellite industry towards “SmallSat” development and is becoming ...
none4The ALMASat Microsatellite is the first educational satellite of Alma Mater Studiorum, Universi...
A next generation nanosatellite bus is under development at the University of Toronto’s Space Flight...
none4noIn the Second Faculty of Engineering of the University of Bologna, the Aerospace group in For...
As more organizations look to microsatellite constellations to achieve increasingly diverse goals, s...
This thesis describes the author's contributions to three separate projects. The bus of the NORSAT-...
Satellite design, development, fabrication, testing and entry into service is a complex process. Eac...
The Sapienza Space Systems and Space Surveillance Laboratory (S5Lab) of La Sapienza University of Ro...
Low-cost microsatellites structures represent an extremely interesting challenge and a excellent tec...
[[abstract]]One of the main advantage of microsatellites is their small size. The reliability, safet...
Mass reduction is a primary design goal pursued in satellite structural design, since the launch cos...
NORSAT-1 is a multi-payload microsatellite mission funded by the Norwegian Space Center, with three ...
NORSAT-2 is a 16-kilogram microsatellite designed, constructed and tested at the University of Toron...
There is an increasing need for monitoring and regulation of maritime vessels. This regulation can h...
The rapid development of small satellite technologies and the lowering cost of launch services have ...
An evolution is undergoing in the satellite industry towards “SmallSat” development and is becoming ...
none4The ALMASat Microsatellite is the first educational satellite of Alma Mater Studiorum, Universi...
A next generation nanosatellite bus is under development at the University of Toronto’s Space Flight...
none4noIn the Second Faculty of Engineering of the University of Bologna, the Aerospace group in For...
As more organizations look to microsatellite constellations to achieve increasingly diverse goals, s...
This thesis describes the author's contributions to three separate projects. The bus of the NORSAT-...
Satellite design, development, fabrication, testing and entry into service is a complex process. Eac...
The Sapienza Space Systems and Space Surveillance Laboratory (S5Lab) of La Sapienza University of Ro...
Low-cost microsatellites structures represent an extremely interesting challenge and a excellent tec...
[[abstract]]One of the main advantage of microsatellites is their small size. The reliability, safet...
Mass reduction is a primary design goal pursued in satellite structural design, since the launch cos...