Юдинцев В. В.
Научно-технический журнал, №8-9, 2015, с. 10-15
Publication year: 2015

The paper deals with the process of separating a CubeSat from a deployer. The equations of the motion of a CubeSat in the CubeSat deployerare developed. The influence of the parameters of the CubeSat and the parameters of the CubeSat deployer to the angular velocities of the CubeSat is investigated. The recommendations are made to reduce the angular velocity of the CubeSat.