We have begun the feasibility study to build a small satellite in the 3kg mass range and in the power range less than 30W since October in 1998, sponsored by National Space Development Agency of Japan (NASDA). This satellite installs three reaction wheels for an attitude control and camera which will demonstrate optical navigation experiment by using image processing. The BBM design status is described in this paper. The components such as a small reaction wheel, electric flash and onboard computer were built. Mothership - daughtership technology and formation flying experiments are planned. New electric propulsion is being developed for small satellite
Project objectives The proposed research is part of a national project (coordinated by the Universit...
Currently the GN&C’s Propulsion Branch of the NASA’s Goddard Space Flight Center (GSFC) is conductin...
The introduction of the Cubesat standard, together with both miniaturization and improved performanc...
The goal of the research program is to develop a prototype of a satellite constellation consisting o...
AbstractThe article describes nanosatellite SamSat-218D designed in Samara State Aerospace Universit...
Nowadays, it is widely used the term Nanosatellite when we refer to those satellites whose mass are ...
Nanosatellite refers to an artificial satellite that has a mass of less than 10 kg and small dimensi...
Development of small satellites has presented a great opportunity for research institutes to join sp...
Demand of an environment test facility suitable for micro/nano satellites has increased as the numbe...
Recent nanosatellite programs and studies of nanosatellites for operational missions have highlighte...
Recently, there has been an increased interest in using nanosatellites in space science missions due...
It has frequently been proposed to use very small nanosatellites for missions requiring orbital agil...
The scientific understanding of key physical processes between the Sun and Earth require simultaneou...
Nanosatellites represent an emerging opportunity to pursue a broad set of mission goals, including r...
This paper highlights the mission, design and development of the 2U CubeSat AOBA VELOX-IV by Nanyang...
Project objectives The proposed research is part of a national project (coordinated by the Universit...
Currently the GN&C’s Propulsion Branch of the NASA’s Goddard Space Flight Center (GSFC) is conductin...
The introduction of the Cubesat standard, together with both miniaturization and improved performanc...
The goal of the research program is to develop a prototype of a satellite constellation consisting o...
AbstractThe article describes nanosatellite SamSat-218D designed in Samara State Aerospace Universit...
Nowadays, it is widely used the term Nanosatellite when we refer to those satellites whose mass are ...
Nanosatellite refers to an artificial satellite that has a mass of less than 10 kg and small dimensi...
Development of small satellites has presented a great opportunity for research institutes to join sp...
Demand of an environment test facility suitable for micro/nano satellites has increased as the numbe...
Recent nanosatellite programs and studies of nanosatellites for operational missions have highlighte...
Recently, there has been an increased interest in using nanosatellites in space science missions due...
It has frequently been proposed to use very small nanosatellites for missions requiring orbital agil...
The scientific understanding of key physical processes between the Sun and Earth require simultaneou...
Nanosatellites represent an emerging opportunity to pursue a broad set of mission goals, including r...
This paper highlights the mission, design and development of the 2U CubeSat AOBA VELOX-IV by Nanyang...
Project objectives The proposed research is part of a national project (coordinated by the Universit...
Currently the GN&C’s Propulsion Branch of the NASA’s Goddard Space Flight Center (GSFC) is conductin...
The introduction of the Cubesat standard, together with both miniaturization and improved performanc...