The CoolerSat is a prototype intended to introduce new team members to the team structure, and to give the team experience as we move toward high-altitude balloon testing of components and subsystems in the summer. These components will eventually be flown on a mission to low earth orbit on a 1-U CubeSat
CubeSats are small satellites with a standardized size of 10 cm x 10 cm x 10 cm (1U). The satellites...
As CubeSat and SmallSat missions increase in complexity and power consumption they present innate th...
The paper deals with the mission analysis and conceptual design of an interplanetary 6U CubeSats sys...
The Missouri University of Science and Technology Satellite Research Team began its high-altitude ba...
The Experiment for X-ray Characterization and Timing (EXACT) mission is a 3U CubeSat technology-deve...
The design and analysis of an environmental control system developed for a balloon-borne electronics...
While building and launching a CubeSat is lower in cost compared to a standard satellite, verifying ...
Cubesat 5000 is designed for the annual Physics weather balloon launch which is done for the senior ...
The ODU CubeSat is part of a multi-university collaborative project that aims to build a constellati...
During the summer of 2010, our team developed a thermoelectric cooler control system as part of the ...
Cube Satellite (CubeSat) launches have been on the rise since its first launch in2003. This populari...
CubeSat technology, although a young member of the space craft family, has proven to be a multipurpo...
ARKSAT-1 is a 1U CubeSatellite developed at the University of Arkansas (UA). The primary mission of ...
The addition of a weather ballooning program at Western Oregon University creates research opportuni...
Spanning an altitude range from 20 – 1000 km, the Earth’s middle and upper atmosphere forms the inte...
CubeSats are small satellites with a standardized size of 10 cm x 10 cm x 10 cm (1U). The satellites...
As CubeSat and SmallSat missions increase in complexity and power consumption they present innate th...
The paper deals with the mission analysis and conceptual design of an interplanetary 6U CubeSats sys...
The Missouri University of Science and Technology Satellite Research Team began its high-altitude ba...
The Experiment for X-ray Characterization and Timing (EXACT) mission is a 3U CubeSat technology-deve...
The design and analysis of an environmental control system developed for a balloon-borne electronics...
While building and launching a CubeSat is lower in cost compared to a standard satellite, verifying ...
Cubesat 5000 is designed for the annual Physics weather balloon launch which is done for the senior ...
The ODU CubeSat is part of a multi-university collaborative project that aims to build a constellati...
During the summer of 2010, our team developed a thermoelectric cooler control system as part of the ...
Cube Satellite (CubeSat) launches have been on the rise since its first launch in2003. This populari...
CubeSat technology, although a young member of the space craft family, has proven to be a multipurpo...
ARKSAT-1 is a 1U CubeSatellite developed at the University of Arkansas (UA). The primary mission of ...
The addition of a weather ballooning program at Western Oregon University creates research opportuni...
Spanning an altitude range from 20 – 1000 km, the Earth’s middle and upper atmosphere forms the inte...
CubeSats are small satellites with a standardized size of 10 cm x 10 cm x 10 cm (1U). The satellites...
As CubeSat and SmallSat missions increase in complexity and power consumption they present innate th...
The paper deals with the mission analysis and conceptual design of an interplanetary 6U CubeSats sys...