CLIMB is a 3U CubeSat whose goal is to reach the Van Allen belt with the help of an advanced propulsion system. Usually, the Van Allen radiation belt is avoided by spacecraft due to its high radiation levels. CLIMB aims exactly for this region to conduct various measurements. The spacecraft’s subsystems need to be designed in a way to cope with this rough environment and to ensure that even in case of failure or loss of the spacecraft, it still shall deorbit within 25 years, as required by the Austrian Space Law. Some of the systems of CLIMB have already flown and been qualified during the previous Austrian mission PEGASUS
Kyung Hee University (KHU) has been developing a CubeSat for the space science mission called Scient...
CubeSats are small satellites with a standardized size of 10 cm x 10 cm x 10 cm (1U). The satellites...
Existing and expected debris mitigation regulations require LEO spacecraft to deorbit within 25 year...
Based on its successful CubeSat mission PEGASUS, the University of Applied Sciences Wiener Neustadt ...
This paper defines a mission concept and system design for a 3U CubeSat technology demonstration. Th...
We work on a student 3U Cubesat mission, called JUMPSAT, expected for 2017. This is a collaborative ...
This paper denotes a mission concept and system design for a 3U CubeSat technology demonstration. Th...
The Van Allen belts are said to be a pack of highly energetic particles which are extremely fatal to...
Cubesats have emerged as powerful tools for a new class of space missions that is recognized by acad...
The InflateSail (QB50-UK06) CubeSat, designed and built at the Surrey Space Centre (SSC) at the Univ...
A volunteer consortium of the individuals and organizations listed on the title page of this documen...
The paper deals with an interplanetary CubeSats mission to Earth-Sun Libration point. CubeSats are a...
The paper deals with the mission analysis and conceptual design of an interplanetary 6U CubeSats sys...
The paper deals with an interplanetary CubeSats mission to Earth-Sun Libration point. CubeSats are a...
We introduce a joint research project that stems from the international collaboration between Polyte...
Kyung Hee University (KHU) has been developing a CubeSat for the space science mission called Scient...
CubeSats are small satellites with a standardized size of 10 cm x 10 cm x 10 cm (1U). The satellites...
Existing and expected debris mitigation regulations require LEO spacecraft to deorbit within 25 year...
Based on its successful CubeSat mission PEGASUS, the University of Applied Sciences Wiener Neustadt ...
This paper defines a mission concept and system design for a 3U CubeSat technology demonstration. Th...
We work on a student 3U Cubesat mission, called JUMPSAT, expected for 2017. This is a collaborative ...
This paper denotes a mission concept and system design for a 3U CubeSat technology demonstration. Th...
The Van Allen belts are said to be a pack of highly energetic particles which are extremely fatal to...
Cubesats have emerged as powerful tools for a new class of space missions that is recognized by acad...
The InflateSail (QB50-UK06) CubeSat, designed and built at the Surrey Space Centre (SSC) at the Univ...
A volunteer consortium of the individuals and organizations listed on the title page of this documen...
The paper deals with an interplanetary CubeSats mission to Earth-Sun Libration point. CubeSats are a...
The paper deals with the mission analysis and conceptual design of an interplanetary 6U CubeSats sys...
The paper deals with an interplanetary CubeSats mission to Earth-Sun Libration point. CubeSats are a...
We introduce a joint research project that stems from the international collaboration between Polyte...
Kyung Hee University (KHU) has been developing a CubeSat for the space science mission called Scient...
CubeSats are small satellites with a standardized size of 10 cm x 10 cm x 10 cm (1U). The satellites...
Existing and expected debris mitigation regulations require LEO spacecraft to deorbit within 25 year...